Student Solutions Manual
for
Modern Physics
Third Edition
Raymond A. Serway
Professor Emeritus, James Madison University
Clement J. Moses
Professor Emeritus, Utica College of Syracuse University
Curt A. Moyer
University ofNorth Carolina-Wilmington
T H O M S O N
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Contents
Chapter 1: Relativity I
Chapter 2: Relativity II
Chapter 3: The Quantum Theory of Light
Chapter 4: The Particle Nature of Matter
Chapter 5: Matter Waves
Chapter 6: Quantum Mechanics in One Dimension
Chapter 7: Tunneling Phenomena
Chapter 8: Quantum Mechanics in Three Dimensions
Chapter 9: Atomic Structure
Chapter 10: Statistical Physics
Chapter 11: Molecular Structure
Chapter 12: The Solid State
Chapter 13: Nuclear Structure
Chapter 14: Nuclear Physics Applications
Chapter 15: Particle Physics
f
%
1
Relativity I
1-1
F =—. Consider the special case of constant mass. Then, this equation reduces to FA = maA
at
in the stationary reference system, and v B = v A + vBA where the subscript A indicates that the
measurement is made in the laboratory frame, B the moving frame, and vBA is the velocity of
B with respect to A. It is given that a : = —-^-. Therefore from differentiating the velocity
at
equation, we have aB = a A + aj. Assuming mass is invariant, and the forces are invariant as
well, the Newton's law in frame B should be J]F = maA = maB -mav which is not simply
ma B . So Newton's second law £ F = W 3 B is invalid in frame B. However, we can rewrite it as
X F+maj =ma B , which compares to £ F+mg = m&B. It is as if there were a universal
gravitational field g acting on everything. This is the basic idea of the equivalence principle
(General Relativity) where an accelerated reference frame is equivalent to a reference frame
with a universal gravitation field.
1-3
IN THE REST FRAME:
In an elastic collision energy and momentum are conserved.
jji=m1vli+m2v2i=(03kg)(5
Pt=m1vli+m2v2i
m/s) + (0.2kg)(-3 m/s) = 0.9 kg m/s
This equation has two unknowns, therefore, apply the conservation of kinetic energy
Ei =E{ =—WjUji +—m2v2i =—m1Vif H—m2v2f and conservation of momentum one finds that
Zi
£i
Jl
/U
u lf = -1.31 m/s and v^ = 6.47 m/s or vlf = -1.56 m/s and v^ = 6.38 m/s. The difference in
values is due to the rounding off errors in the numerical calculations of the mathematical
quantities. If these two values are averaged the values are v1{ = -1.4 m/s and o a = 6.6 m/s,
p f =0.9 kg m/s. Thus, y>x =p{.
IN THE MOVING FRAME:
Make use of the Galilean velocity transformation equations. p{ -m^'^+m^o'^; where
v
'\\ ~ vn ~ v'= 5 m/s ~ ( - 2 m/s) = 7 m/s. Similarly, v'2i = -1 m/s and p[ =1.9 kg • m/s. To find
p'f use v'lt = vVl - v and v'2i = v2i-v' because the prime system is now moving to the left.
Using these results give p'{ = 1.9 kg • m/s.
1
CHAPTER 1
RELATIVITY I
This is a case of dilation. T = yT in this problem with the proper time T = T0
-1/2
121V2
L 0 /2
in this case T = 2T0, v = \ 1 •
21V2
Tn=>- =
1-1 f-
r
1 -1 - jl
therefore v = 0.866c.
The problem is solved by using time dilation. This is also a case of v « c so the binomial
„ -,
expansion is used Af = yAt' = 1 + -
2c^
„
Af',Af-Af' =
2c2
,- ; i> =
2c 2 (Af-AO
Af
-,1/9
A* = (24 h/ d a y)( 3 600 s/h) = 86 400 s; At = At' - 1 = 86 399 s;
1/2
2(86 400 s-86 399 s)
v=
86399 s
L
= 0.004 8c = 1.44 xlO 6 m/s.
- ^
^earth
_
^earth
-
2lV2
, L', the proper length so L earth =L = L[l -(0.9) 2 ] 1/2 = 0.436L.
^
At = yAt'
A
„2A _ 1 /2
/
2 \
i+
At = At'
(4.0 xlO 2 m/s) 2
(3 600 s)
2(3.0 xlO 8 m/s)'
= (1 + 8.89 x 10"13 )(3 600 s) = (3 600 + 3.2 x 10~9) s
At - At' ~ 3.2 ns. (Moving clocks run slower.)
(a)
T=yr'=[l-(0.95)2]
(b)
Af•' =
1/2
(2.2/zs) = 7.05//s
d
3 x l 0 3 m , „ 1n _ 5s
.
,
=
= 1.05x10 s, therefore,
0.95c
0.95c
N = N0 expf- —) = (5 x 104 muons) exp(-1.487) -1.128 x 104 muons.
(a)
For a receding source we replace v by —v in Equation 1.15 and obtain:
tic-vf'2
/ob
\[c + vf'
V
1
[1-Vc]1/2
2
V
[ l + l;/c]V2
•"-3K>-
2 >
+ —=
c
Source
/source
—
1
l/i
2
4c
where we have used the binomial expansion and have neglected terms of second and
higher order in - . Thus, -^—
^
/source
= iob
^source = - /source
**
MODERN PHYSICS
1-17
(b)
From the relations f =—,-*- = — T we find — = —'-—dX, or — = —— = —
1
X dX
X2
f
c/X
X
f
c
(c)
Assuming v«c,
(a)
Galaxy A is approaching and as a consequence it exhibits blue shifted radiation. From
7,
21
- fi
u
(550nm) 2 -(450nm) 2
-^source "~o
Example 1.6, p=- = 2| o u r c e 22°bs s o t h a t P:
2- = 0.198. Galaxy
T A
c
I source +
(550nmr + (450nm) z
""
""obs
A is approaching at v = 0.198c.
(b)
For a red shift, B is receding, /3-
— B—— ,or VB\ —— c =
c = 0.050c = 1.5 x 10 m/s.
v
c X
\ X ) V397nm;
6
71
r
32
— ^'
source "obs
i2
-i. I2
source "*" ^obs
SQ
t h a t
_ (700nm) 2 -(550nm) 2 „ „2 3„7 „ „ ,
„.
,.
t
5=
'-z—
V2 = °• Galaxy
2
J B is receding
b at v = 0.237c.
(700nm) +(550nm)
1-19
KjM
= -u „ ; M ^ = 0.7c = .
Mx4
" " , ; 0.70c =
2
1-"XA"XBA '
"
2MX4
1 + ("XA/C)
or OJOwf^ - 2cuXA +0.7c2 = 0.
2
Solving this quadratic equation one finds w ^ = 0.41c therefore u^ = -Ux/i = ~0-41c.
1-21
u'x =
ux-v , . 2
l-uxv/c
1-23
(a)
0.50c-0.80c
. , =-0.50c
l-(0.50c)(0.80c)/c 2
Let event 1 have coordinates x^ - yx = Zj = fj = 0 and event 2 have coordinates
x2 =100 mm, y 2 =z 2 = t2 =0.1n S', x^ = y(x1 -vt1) = Q, y{ =y a = 0 , zj =z x =0,and
..2 "T 1 / 2
t{ = rh-
= 0,with y-
rn
systemS', x'2 = y(x2-vt2)
t'2 = 7h
1-25
and so y = [l -(0.70) 2 ]" 1/2 = 1.40. In
= l'i0 m, y2 = z 2 = 0 , a n d
-\-j:\X2
(1.4)(-0.70)(100 m)
= -0.33//s.
3.00xl0 8 m/s
(b)
Ax' = x 2 - ; t i = 1 4 0 m
(c)
Events are not simultaneous in S', event 2 occurs 0.33 jus earlier than event 1.
We find Carpenter's speed:
mGM
GM l1'2
R + h.
mv2
(6.67x10"" X5.98xlO M )
6.37 x l 0 6 + 0 . 1 6 x l 0 6
1/2
= 7.82 km/s.
2x(R + h) 2^6.53 xlO 6 )
,
Then the period of one orbit is T = =^
'- = — ^ - — - ^ - = 5.25 x 103 s.
7.82x10"
3
4
CHAPTER 1
RELATIVITY I
.2 A -1/2
(a)
The time difference for 22 orbits is At - At' = (y -1)At' =
1-
c2J
- 1 (22)(T).
Using the binomial expansion one obtains
'
(b)
lv2
^
1 + - 2- V - 1 (22)(7>
2- c
7.82 xlO 3 m/s
3 x10 s m/s
(22)(5.5xl0 3 s) = 39.2//s.
39.2 us
For one orbit, At - At' = —'•
= 1.78 //s » 2 //s. The press report is accurate to one
significant figure.
1-27
For the pion to travel 10 m in time At in our frame,
-1/2
10 m = vAt = v{yAt') = u(26 x 10"9 s)
(3.85xl0 8 m/s)"
c2
1.46xlO17 m 2 / s 2 = u 2 ( l + 1.64)
v = 2.37xl0 8 m/s = 0.789c
1-29
(a)
A spaceship, reference frame S', moves at speed v relative to the Earth, whose
reference frame is S. The space ship then launches a shuttle craft with velocity v in
the forward direction. The pilot of the shuttle craft then fires a probe with velocity v
in the forward direction. Use the relativistic compounding of velocities as well as its
inverse transformation: u'=- ur-v
-, and its inverse u = - ur + v
.The above
i-Mc2)
— - - i+(wxv/c2y
variables are defined as: v is the spaceship's velocity relative to S, u'x is the velocity of
the shuttle craft relative to S', and ux is the velocity of the shuttle craft relative to S.
Setting u'x equal to v, we find the velocity of the shuttle craft relative to the Earth to
be: ur =2
l + (o/c)
(b)
"
If we now take S to be the shuttle craft's frame of reference and S' to be that of the
probe whose speed is v relative to the shuttle craft, then the speed of the probe
2v
relative to the spacecraft will be, u'x =
r-. Adding the speed relative to S yields:
1 + {v/c)
\2
3v + v3/c3
3+(p/c)"
. Using the Galilean transformation of velocities, we see
«,=
2
l + 2v2/c2
l + 2(z;/c)
that the spaceship's velocity relative to the Earth is v, the velocity of the shuttle craft
relative to the space ship is v and therefore the velocity of the shuttle craft relative to
the Earth must be 2v and finally the speed of the probe must be 3v. In the limit of low
— , ux reduces to 3v. On the other hand, using relativistic addition of velocities, we
find that ur = c when v —> c.
MODERN PHYSICS
1-31
In this case, the proper time is T0 (the time measured by the students using a clock at rest
relative to them). The dilated time measured by the professor is: At = y T0 where At = T +t.
Here T is the time she waits before sending a signal and t is the time required for the signal
to reach the students. Thus we have: T +t = yT0. To determine travel time t, realize that the
distance the students will have moved beyond the professor before the signal reaches them is:
d v
d = v(T +t). The time required for the signal to travel this distance is: t = — = —(T + t). Solving
c c
for t gives: t
—T 1—
. Substituting this into the above equation for (T +t) yields:
yT0, or T 1 —
= yT0. Using the expression for y this becomes:
-1/2
V2
1+1-1^
-1/2
i-i^
1-33
5
(a)
r0,orT:
*.U-f
'('-7
We in the spaceship moving past the hermit do not calculate the explosions to be
simultaneous. We measure the distance we have traveled from the Sun as
L = LpJl-(-)
= (6.00 ly)Vl -(0.800) 2 = 3.60 ly.
We see the Sun flying away from us at 0.800c while the light from the Sun approaches
at 1.00c. Thus, the gap between the Sun and its blast wave has opened at 1.80c, and
the time we calculate to have elapsed since the Sun exploded is —
— = 2.00 yr. We
see Tau Ceti as moving toward us at 0.800c, while its light approaches at 1.00c, only
0.200c faster. We measure the gap between that star and its blast wave as 3.60 ly and
growing at 0.200c. We calculate that it must have been opening for —
— = 18.0 yr
0.200c
and conclude that Tau Ceti exploded 16.0 years before the Sun
(b)
1-35
Consider a hermit who lives on an asteroid halfway between the Sun and Tau Ceti,
stationary with respect to both. Just as our spaceship is passing him, he also sees the
blast waves from both explosions. Judging both stars to be stationary, this observer
concludes that the two stars blew up simultaneously
In the Earth frame, Speedo's trip lasts for a time At = — =
'•—-— = 21.05 Speedo's age
v
v
v
6
v 0.950 ly/yr
advances only by the proper time interval: At. - — = 21.05 yrVl - 0.95 2 = 6.574 yr during his
7
W
trip.
° l y Vl-0.75 2 = 17.64 yr. While Speedo
K Similarly
y for Goslo, Af_
v = — J l - \2 =
V
v V c
0.750 ly/yr
'
has landed on Planet X and is waiting for his brother, he ages by
20.0 ly
0.750 ly/yr
0.20 ly
/, nnr2 z
,n,A
—Vl-0.75
= 17.64
yr.
0.950 ly/yr
Then Goslo ends up older by 17.64 yr - (6.574 yr + 5.614 yr) = 5.45 yr.
6
CHAPTER 1
RELATIVITY I
1-37
Einstein's reasoning about lightning striking the ends of a train shows that the moving
observer sees the event toward which she is moving, event B, as occurring first. We may take
the S-frame coordinates of the events as (x = 0, y = 0, z = 0, t = 0 ) a n d ( x = 100 m, y = 0, z = 0,
f = 0). Then the coordinates in S' are given by Equations 1.23 to 1.27. Event A is at (x' = 0,
y' = 0,z' = 0,t' = 0). The time of event B is:
1
t' = r\t
vn0.8
l
0 - ^ ( 1 0 0 m) | = 1.667|
80 m
= -4.44xl0"" 7 s.
3x10 s m/s
The time elapsing before A occurs is 444 ns.
1 M
1-39
, >
(a)
- .,
. „.. ^ c
GMEm mv2
mflnrS?
For the satellite 2, f = ma '• , — =
=—
r
r
r \ T J
GMET'=4/rr
.2.3
1/3
6.67X10-11 N-m 2 (5.98xlO a * kg)(43080s)
= 2.66x10' m
2A~2
kg 4/r
(b)
(c)
2^(2.66 xlO 7 m)
27tr
v—
43080 s
= 3.87xl0 3 m/s
The small fractional decrease in frequency received is equal in magnitude to the
fractional increase in period of the moving oscillator due to time dilation:
fractional change i n / = -(y-1)
= -
^-(S^xloVSxlO 8 )
f 3.87 xlO 3 ^ 2
1
= 1- (,1 2
— —
\ 3x10°
I
(d)
= -8.34x10""
The orbit altitude is large compared to the radius of the Earth, so we must use
GMEm
U.
s
~
6.67 x l 0 ~ " N m ^ W S x l O 2 4 kg)m
6.67x10"" N m ^ S x l O 2 4 kg)m
kg22.66xl07m
kg 2 6.37xl0 6 m
= 4.76xl0 7 J/kgm
A / _ A U g _ 4 . 7 6 x l 0 7 m 2 /s 2
/ ~ rnc2 ~ ( 3 x i o 8 m/s) 2
(e)
,-1
= +5.29x10 -10
-8.34 x 10""" + 5.29 x 10""10 = +4.46 x 10 -10
2
Relativity II
2-1
p=
mv
2
[l-(, /c2)f2
(l.67xl0 _27 kg)(0.01c)
(a)
2 V2
:5.01xl0 -21 kg m/s
[l-(0.01c/c) ]
(b)
(l.67xl0 _27 kg)(0.5c)
^ — = 2.89xl0 _ w k g m / s
2
[l-(0.5c/c) ]
(c)
(l.67xl0- 27 kg)(0.9c)
P
r
f w ^ =1-03x10-18 k g m / s
[l-(0.9c/c) 2 ] 7
(d)
1.00 MeV
13
1.602x10"" J
2.998x10" m/s
5.34 x 10 ^ kg • m/s so for (a)
(5.01 xlO - 2 1 kgm/s)(100 MeV/c)
5.34 xlO - 2 2 kg m/s
= 9.38 MeV/c
SimUarly, for (b) p = 540 MeV/c and for (c) p = 1930 MeV/c.
2-3
As F is parallel to v, scalar equations are used. Relativistic momentum is given by
p = ymv =
y=-, and relativistic force is given by
l-(v/cf]2lV2 '
mv
dt
F=
dt
dp
dt
[[M'AOTJ
m
cfo
[l-(t, 2 / c 2 )fHd£
7
10
CHAPTER 2
RELATIVITY II
2-17
Am = mRa - m ^ - m He (an atomic unit of mass, the u, is one-twelfth the mass of the 12C atom
or 1.660 54xlCT27 kg)
Am = (226.025 4 - 22.017 5 - 4.002 6) u = 0.005 3 u
£ = (Am)(931 MeV/u) = (0.005 3 u)(931 MeV/u) = 4.9 MeV
2-19
Am = 6mp + 6m„ - m c = [6(1.007 276) + 6(1.008 665) -12] u = 0.095 646 u,
AE = (931.49 MeV/u)(0.095 646 u) = 89.09 MeV.
Therefore the energy per nucleon =
2-21
/E,
e(-)
89 09 MeV
= 7.42 MeV.
12
p
e(+)
O— O
K, p(e-) positron
at rest
Conservation of mass-energy requires K + 2mc2 = 2E where K is the electron's kinetic energy,
m is the electron's mass, and E is the gamma ray's energy.
E = — + mc2 = (0.500 + 0.511) MeV = 1.011 MeV.
2
Conservation of momentum requires that pe = 2p cos 6 where p _ is the initial momentum of
£
the electron and p is the gamma ray's momentum, — = 1.011 MeV/c. Using
c
E2. = p\.c2 + {mc2) where Ee_ is the electron's total energy, E - -K + mc2, yields
P
_=iVi^W ^
e
0 0 ) 2
c
^-OPXasii) MeV =1
m
c
Finally, cos 0 = ^ - = 0.703; 9 = 45.3°.
2p
2-23
In this problem, M is the mass of the initial particle, mx is the mass of the lighter fragment, vx
is the speed of the lighter fragment, mh is the mass of the heavier fragment, and vh is the
speed of the heavier fragment. Conservation of mass-energy leads to
Mc 2 =-
^
•
^
^w ^W
MODERN PHYSICS
:
The time of flight is At = — =
—-,
= 7.04 x 10 -8 s. The current when electrons are
6
6
v 3.98 xlO m/s
2 8 c m a p a r t i s J = ^ = — = I 6 x l ° " I "-8C = 2 . 2 7 x l 0 - 1 2 A .
t At 7.04xlO s
39
6
Quantum Mechanics in One
Dimension
6-1
6-3
(a)
Not acceptable - diverges as x -» °°.
(b)
Acceptable.
(c)
Acceptable.
(d)
Not acceptable - not a single-valued function.
(e)
Not acceptable - the wave is discontinuous (as is the slope).
(a)
ylsinf—1 = Asin(5xl010x) so f ^ l = 5xl0 10 m"1, / l = - ^ - = 1.26xl0-10 m.
n \
(b)
(c)
w
3
h'* O.lMlO
6.626 AxlO~
J.U
l*Js_
»
_ e_^, w , n
. , -24
.,-24 l
/
M
-10
p =X
- r = 1.26
———__^-2_
5,26x10
kg
m/s
xlO m =
K = -£- m = 9.11xl{T31kg
6
2m
2
( S ^ x l O ^ k g m / sv )
._
K = *-.
*
( = 1.52 x 10"17 J
_31
(2x9.11xl0 kg)
152x n
K= 1.6xlO"
Z19 J/eV =95 eV
6-5
(a)
Solving the Schrodinger equation for U with E = 0 gives
u=l —-(£)
2mJ y
If ^ = AT**/*-2 t h e n ^ = ( 4 A x 3 - 6 A x L 2 ) ^ e - ^ 2 ,
41
Z'
U
=
fc2
V4x2
2
2mL A L2
-6 .
CHAPTER 6
QUANTUM MECHANICS IN ONE DIMENSION
•at*
(b)
U(x) is a parabola centered at x - 0 with 17(0) =
~- < 0:
mL
Since the particle is confined to the box, Ax can be no larger than L, the box length. With
n = 0, the particle energy E„ =
n1.V7j - is also zero. Since the energy is all kinetic, this implies
8mL
\p\\ = 0. But (px) = 0 is expected for a particle that spends equal time moving left as right,
giving A px = y(p 2 ) - {px)2 ~ 0 • Thus, for this case A pxA x = 0, in violation of the uncertainty
principle.
fc„ =
^-, so A £ = £ 2 _ cj =
8mL2
8mL2
(1240 eV nm/c)2
A£ = (3)
- = 6.14MeV
8(938.28 xlO 6 eV/c2)(lO~5 nm) :
he
1240 eV nm
= 2.02x10^ nm
A£ 6.14xl0 6 eV
This is the gamma ray region of the electromagnetic spectrum.
In the present case, the box is displaced from (0, L) by —. Accordingly, we may obtain the
wavefunctions by replacing x with x — in the wavefunctions of Equation 6.18. Using
sin
tin
_L
T
= sin
nit = sin| nnx 1 cos
~2
nnx\
L
L
we get for — < x < —
5
2
2
cos'
¥ M
* '[i
. (nn
(f)-C°{ —L J sinV—2
nnx
2V/2 . f2nx
S
H L
;P2(x):
sin
2i
nx
2nx
L
i(2>7tx
'''HiTH^rhn-tiWrt
MODERN PHYSICS
6-13
(a)
43
10
Proton in a box of width L = 0.200 n m = 2 x 10~,u m
(6.626 x 10"34 J s) 2
E,=
8mpL2
8(1.67 x 10"27 kg)(2 x 10"10 m)'
- = 8.22x10'^ J
8.22 xlO - 2 2 J
= 5.13xlO""3 eV
1.60xlO"19 J/eV
(b)
Electron in the same box:
(6.626 x 10 -34 J s) 2
Ei
8w e L
= 1.506xlO"10 J = 9.40eV.
(c)
The electron has a much higher energy because it is much less massive.
(a)
17 =
(b)
K = 2Ej =
(c)
(+7/3)e2k
rfE
E = U + K and —— = 0 for a minimum
da
d2
„2
6-15
-18
8(9.11 x 10"31 kg)(2xlO -10 m)
'- 1-.+ 1 1 + ( - 1t +
4ne0dj
2 3V
2
2hz
8mx9d 2
3/i z
(7)(l8kezm)
36md2
UmA*
or d = 42mke2
(6.63xlO -34 J s ) 2
<7 =
(42)(9.11xl0"
(d)
(-7/3)e2 _ (-7/3)fce2
4ne0d
M"
A
31
9
kg)(9xl0 N m
2
2
CT )(l.6xlO-
19
= 0.5xlO" 10 m = 0.050 nm
C)
.. . iv/TZ
Nm
3
Since the lithium spacing is a, where Na - V and the density is
where m is the
mass of one atom, we get
1/3
fVm^3
( m Y'~ [.„
7
1n_27l
a
« = \Nm)
ITT-I
= 1^density)
—
=11.66x10
k
g
x
{
"
" ° 530kg/m 3
= 0.28 nm
1/3
m= 2.8xlO -10 m
(2.8 times larger than 2d)
6-17
(a)
The wavefunctions and probability densities are the same as those shown in the two
lower curves in Figure 6.16 of the text.
(b)
p1=
3.5 A
f |yf<fc=
IJA
2
*
35 A
r
. l nx
f sin22 — \dx
ioAj A
UO
x
2
10 . (nx
sin
4?r
3.5
1.5
CHAPTER 6
(a)
QUANTUM MECHANICS IN ONE DIMENSION
Normalization requires
1 = ]\V\2dx = C2 ]{V\ + ¥l}{¥,
+
¥l}dx
= C2{l\iyl\2dx + j\ys2\2dx + jv2¥ldx+jwW2<ix}
The first two integrals on the right are unity, while the last two are, in fact, the same
integral since y/y and y/2 are both real. Using the waveforms for the infinite square
well, we find
^
2
^ ^ =| j s i r ( ^ ) s i n ( ^ ) ^ = Ij{cos^)-coS(^)}ix
where, in writing the last line, we have used the trigonometric exponential identities
of sine and cosine. Both of the integrals remaining are readily evaluated, and are zero.
Thus, 1 = C 2 {l+0 +0 + 0} = 2C2, or C = -^=r. Since y/l2 are stationary states, they
V2
develop in time according to their respective energies Ej 2 as e~'Et^n. Then
V(x, t)=Cfae'W
+ W ^ } .
(c)
*F(;r, t) is a stationary state only if it is an eigenfunction of the energy operator
[E] = ih—. Applying [£] to ¥ gives
of
Since E1#E2, the operations [£] does not return a multiple of the wavefunction, and
so *P is not a stationary state. Nonetheless, we may calculate the average energy for
this state as
(£> = jY[Ef¥dx = C2 \{¥yiE^h
+ ¥2e+iE^h}{ElWie-iE^''
+£ 2 ^ 2 e- E ^}rfx
^{E.Wvtfdx+E^yftfdx}
with the cross terms vanishing as in part (a). Since y/12 are normalized and C 2
we get finally ( £ ) = £ l + £ 2 .
1
7
Tunneling Phenomena
7-1
The reflection coefficient is the ratio of the reflected intensity to the incident wave
(a)
intensity, or R ••i(i/2)(i-or , B u t | l - i p = ( l - i ) ( l - 0 * = ( l - 0 ( l + 0 = |l+il =2,sothat
.••J 2
|(l/2)d+0|
R = 1 in this case.
(b)
To the left of the step the particle is free. The solutions to Schrodinger's equation are
(ImE V^2
e±,kx with wavenumber k = | ——
| . To the right of the step U(x) = U and the
\ h2 )
d
equation is
V_2mnT
,
dx
k = ^V-Vf.
(c)
h
_ , . __.
, .__
_
,
dV_.2
c
, (U-E)ys(x). With y/(x) = e"",b we find
— f = k^y^x), so that
dx
-,1/2
S u b s t i t u t i n g ^ ^ f shows that
For 10 MeV protons, £ = 10 MeV and m =
:
—=
c
(W-E).
E
1
= i1 or —= —.
U 2
. Using
h = 197.3 MeV fm/c(l fm = 10"15 m), we find
h
197.3 MeV fm/c
= 1.44 fm.
1/2
k (2mE)1/2 [(2)(938.28MeV/c2)(10MeV)]
*4 =
7-3
With E = 25 MeV and U = 20 MeV, the ratio of wavenumber is
k,
(
(V5-1) 2
E Y / 2 ( 25 \V2
= V5 = 2.236. Then from Problem 7-2 R:
= 0.146 and
E-tl
25-20
(V5+1) 2
T = 1 - R = 0.854. Thus, 14.6% of the incoming particles would be reflected and 85.4% would
be transmitted. For electrons with the same energy, the transparency and reflectivity of the
step are unchanged.
7-5
(a)
The transmission probability according to Equation 7.9 is
[ImiU-E)]1'2
W
sinh 2 oL with a - L ""' v ~——-—. For E « U, we find
-=1+
j-t;j
h
T(E)
mu-E)
2mUL2 _ , i__.^__ _«___;_ n
.... _,_,_ „. 1 ,aL
» 1 by hypothesis. Thus, we may write sinh ah r-—e . Also
(aiy »
2
=1+(
\e2aL ~ f
)e2aL and a probability for transmission
T(E)
V16E7
V16E/
P=r(E)=(^)e-2^.
U - E = U, giving
49
50
CHAPTER 7
(b)
TUNNELING PHENOMENA
Numerical Estimates: {h = 1.055 x 1(T34 Js)
For m = 9.11 xl(T 3 1 kg, If - E = 1.60 x 10~21 J,L = 10~10 m;
1)
^ = [ 2 m ( t J " E ) ] V 2 = 5.12xl0 8 m"1 and e'2aL =0.90
h
For m = 9.11 x 10~31 kg, 17 - E = 1.60 x 10"19 J,L = 10~10 m; a = 5.12xl0 9 m _1
and e'2at= 0.36
Form = 6.7xl0 - 2 7 kg, U - E = 1.60 x 10~13 J,L = 10 -15 m; a = 4.4xl0 14 m - 1
and e -2aL 0A1
For m = 8 kg, U- E = 1 J, L = 0.02 m; a = 3.8 x 1034 m _1 and
e-2^=g-i.5xio
7-7
«
- 0
The continuity requirements from Equation 7.8 are
A+B=C+D
continuity of *P at x = 0]
ikA-ikB = aD-ctC
aL
Ce- +De
+aL
continuity of
=Fe'*
at x = 0
ox
continuity of 4* at x = L]
L
aDe+al-aCe-aL=ikFeikL
continuity of
at x = L
ax
To isolate the transmission amplitude —, we must eliminate from these relations the
A
unwanted coefficients B, C, and D. Dividing the second line by ik and adding to the first
eliminates B, leaving A in terms of C and D. In the same way, dividing the fourth line by a
and adding the result to the third line gives D (in terms of F), while subtracting the result
from the third line gives C (in terms of F). Combining these results finally yields A:
2-| £ + * " e +aL + 2 + | — + —• -aL The transmission probability is T =
-ft'.«£
M; or
Making use of the identities e
A2
2
2coshaL+f
F
=lJ
7-11
= cosh ah ± sinh ah and cosh ah = 1 + sinh orL, we obtain
]sinhorL
a)
U-E
U-E
cosh2 ah +
ip-
2
2
- + 2 sinh ah = 1 +
sinh a L
or
1r u
i sinh 2 or!
4 E(LZ-E)
(a)
The matter wave reflected from the trailing edge of the well (x = L) must travel the
extra distance 2L before combining with the wave reflected from the leading edge
(x = 0). For A2 = 2L, these two waves interfere destructively since the latter suffers a
phase shift of 180° upon reflection, as discussed in Example 7.3.
(b)
The wave functions in all three regions are free particle plane waves. In regions 1 and
3 where U(x) = U we have
V(x, t) = Aei{k'x-°>t} + Bei{-k'x-°lt)
i{k x
t
i{ k x
«P(x, t) = Fe ' -°' '> + Ge - ' -^
x<0
x<0
MODERN PHYSICS
with k' =
51
. In this case G = 0 since the particle is incident from the left.
In region 2 where U(x) - 0 we have
V(x, t) = Cei{-kx-°") + Dei(kx~m>)
0<x<L
with k =
= — = — for the case of interest. The wave function and its slope
h
A2 L
are continuous everywhere, and in particular at the well edges x = 0 and x = L. Thus,
we must require
A+B=C+D
continuity of *P at x = 0]
k'A-k'B = kD-kC
continuity of — — at x = 0
ox
continuity of ¥ at x = L]
Ce"*L+DeM-=Fe'*'L
fcDe*L -kCe~ikL = k'Feik%
continuity of — — at x = L
ox
„±ikL
For kh = n, e ' = -1 and the last two requirements can be combined to give
kD - kC = k'C + k'D. Substituting this into the second requirement implies
A - B = C + D, which is consistent with the first requirement only if B = 0, i.e., no
reflected wave in region 1.
7-13
As in Problem 7-12, waveform continuity and the slope condition at the site of the delta well
demand A + B = F and ik(A - B) - ikF = - —^- F. Dividing the second of these equations by ik
(2mS/h2)F
and subtracting from the first gives 2B + F = F+
ik
Thus, the reflection coefficient R isR(E) =
T(E) from Problem 7-12, T(E) - 1 +
7-15
-En
-l
fmS\
f-EnV2
, or B = -i —r- F = -iF\ — \h kJ - l
\ E
-E0
. Then, with
1+
if
, we find R(E) + T(E) = [l—2-
i + l -fi
Divide the barrier region into N subintervals of length Ax - xM - xt. For the barrier in the i
subinterval, denote by Ai and F, the incident and transmitted wave amplitudes, respectively.
2
The transmission coefficient for this interval is then 7}
2
T(E) =
r
N
. Now consider the product flT, = T{T2T3...TN •
, and that for the entire barrier is
\h\
|FS
,2V
|F3|2
lArAi^rAi^
Vl-^Nl
Assuming the transmitted wave intensity for one barrier becomes the incident wave intensity
2
for the next, we have |F[|2 =\A2\2, \F2\2 = \A3\2 etc., so that T(E) •-
= Ti r 2 T 3 ... TN. Next, we
assume that Ax is sufficiently small and that U(x) is sensibly constant over each interval (so
that the square barrier result can be used for T,), yet large enough to approximate sinha,Ax
1/2
•, —
1 ea AX
,
, value
,
,
, ith subinterval:
,•
, or.- ---—
[ 2j "(II.--E)]
1
with
' , where
a,-, •is the
taken
by a •in the
—!
—.
2
'
h
52
CHAPTER 7
TUNNELING PHENOMENA
U
U
,2«;AX
Then,— = 1 +
and the transmission coefficient
sinh 2 (a,Ax) =
4£(U,-E)
16E(U,-E)
T;
16E(U,-E) -2a,&x I _ ni6E(L7,-E)
for the entire barrier becomes T(E) = n
e- r a *' t o .To
U
LT,2
recover Equation 7.10, we approximate the sum in the exponential by an integral, and note
that the product in square brackets is a term of order 1: T(E) ~ eZ2cCitiX = e '
2m[U(x)-E]1'2
a(x) = :
7-17
ax
x
where now
The collision frequency/is the reciprocal of the transit time for the alpha particle crossing the
v
nucleus, or / = — , where v is the speed of the alpha. Now v is found from the kinetic energy
2R
which, inside the nucleus, is not the total energy E but the difference E-U between the total
energy and the potential energy representing the bottom of the nuclear well. At the nuclear
radius R = 9 fm, the Coulomb energy is
fc(Ze)(2e)
• 2Z
R
a
°-1 = 2(88X27.2 eV)[ 5 2 9 x l °
R
9fm
fa
| = 28.14 MeV.
From this we conclude that U = -1.86 MeV to give a nuclear barrier of 30 MeV overall. Thus
an alpha with E = 4.05 MeVhas kinetic energy 4.05 +1.86 = 5.91 MeV inside the nucleus. Since
the alpha particle has the combined mass of 2 protons and 2 neutrons, or about
3 755.8 MeV/c 2 this kinetic energy represents a speed
2E_,V/2
v= m
2(5.91)
3 755.8 MeV/c 2 _
Thus, we find for the collision frequency / =
v
2R
1/2
= 0.056c.
0.056c
= 9.35xl0 2 0 Hz
2(9 fm)
8
Quantum Mechanics in Three
Dimensions
8-1
E=
r
h2n2
2m
\2
r
\
Viz
\Ly J
2
Lx =L, Ly =LZ =2L.Let
h rc2
j - = E 0 .Then E = E0(4«i +n2+n3).
8mL
Choose the quantum
numbers as follows:
E
"l
«2
1
1
1
2
1
2
2
2
1
1
1
2
1
1
2
1
2
2
1
3
"3
1
1
2
1
2
2
1
2
3
1
6
9
9
18
12
21
21
24
14
14
*
*
ground state
first two excited states
*
next excited state
*
*
next two excited states
Therefore the first 6 states are y/m, y/m, ipn2, W\n> ¥mr and y/m with relative energies
— = 6,9,9,12,14,14. First and third excited states are doubly degenerate.
8-3
nL=\\
( fc2*r2 "\
(a)
(b)
E=
n2 =
2mL )
n, n,
1
1
1 3
3
1
2
11
ml2
n.
3
1 3-fold degenerate
1
53
CHAPTER 8
(c)
QUANTUM MECHANICS IN THREE DIMENSIONS
7t\i\
(3nz
(/„ 3 = /lsinf-^Jsin( - • 'sin
„ . (xx\
. .
(a)
(b)
LJ
U
. Ciay\ . (KZ
(3KX\
. (7cy\ .
(KZ
3h2
3(6.63 xlO" 34;) 2
„
m = « 2 = n 33 = 1 and E m = - ^ - y2 =
i
__..
„2 8. = 2.47x 1CT13 J -1.54 MeV
27
8mL
8(1.67 xl0" )(4xl0- )
(22+l2+l2)h2
States 211,121,112 have the same energy and £ = —•— = 2Em « 3.08 MeV
Smite2+22+l2)/z2
and states 221,122,212 have the energy E = r—-— = 3E U1 = 4.63 MeV.
8mL
(c)
Both states are threefold degenerate.
The stationary states for a particle in a cubic box are, from Equation 8.10
«F(x, y, z, t) = Asin(fc1^)sin()t2y)sin(fc3z)e~''£(/'i
= 0 elsewhere
0< x, y, x<L
where kt = —3—, etc. Since 4* is nonzero only for 0 < x <L, and so on, the normalization
condition reduces to an integral over the volume of a cube with one corner at the origin:
l=ldxjdyjdz\V(r,
ft
L
L
tf = A2 U sin2 (k^dxj sin2 (k2y)dyj sin2 (k3z)dz
lo
0
0
L
L
L I
Using 2sin 2 # = l - c o s 2 # gives jsin2(k1x)dx =
sin(2fcjx) . ButfcjL= nxn, so the last
o
^ 4KJ
o
term on the right is zero. The same result is obtained for the integrations over y and z. Thus,
{L\3
(2\^2
2
normalization requires l = A \-\
otA= for any of the stationary states. Allowing the
edge lengths to be different at Llr L2, and L3 requires only that L3 be replaced by the box
volume L1L2L3l in the final result: A -
if 2 Y 2 Y 2 ^11//2 (
8
V^2 ^ 8 \^2
, where
lA^l A^2 A^3 J)
\L1L2L3 J
\V>
V - L^LT, is the volume of the box. This follows because it is still true that the wave must
vanish at the walls of the box, so that fcjLj = nxn, and so on.
4.714 xlO- 34 Js = [/(Z + l)]V2
6.63 xKT 34 Js
2K
(4.714 xl0 _34 ) 2 (2/zr) 2
Z(Z + 1) = '—,
^ l ^ x l O 1 =20 = 4(4 + 1)
(6.63 xlO' 3 4 ) 2
so / = 4 .
MODERN PHYSICS
8-11
(a)
L = [l(l + l)]l/zh;
4.83xl0 3 1 Js = [KZ + D] 1/2 fc,so
(4.83 xlO 3 1 J s f
.
„,2
,
l +l = -±
^ - T = (4.58xl0 65 ) =l2
(1.055 x l O ^ J s ) 2 V
'
65
Z = 4.58xl0
,
2
(b)
8-13
WithL = m weget AL-ft and — - j = 2.18x 10"66
Z = 2forHe+
(a)
For n = 3,1 can have the values of 0,1,2
Z = 0 -> m,=0
1 = 1 -» m, = - 1 , 0, +1
1 = 2 -> m, = -2, - 1 , 0, + 1 , +2
(b)
All states have energy £ 3 = —;j-(13.6 eV)
E 3 =-6.04eV.
8-15
(a)
£„=-
'fa> 2 Yz 2 ^
2a n A n
V-*"o
from Equation 8.38. But a 0 =
r- so with m e -» // w e get
m e te z
2„4 V - 7 2 \
£„ = •
(b)
2fc 2
fcc / * V Z Z ( 1 _ 1 w i t h
Forn = 3 - » 2 , E33 - E 2 = — =
~T 4"1
^ = 656.3 n m f o r H (Z = l ,
1
~ x'
ju^me).For
8-17
v«2;
m
656.3
H e + , Z = 2 , a n d ju = me, so, X =—^ = 164.1 n m (ultraviolet).
(c)
For positronium, Z = 1 a n d ju = m„
—-, so, X = (656.3)(2) = 1312.6 n m (infrared).
(a)
For a d state, Z = 2
L = [J(l + l)]V2ft = (6)V 2 (l.055xl0- 3 4 Js) = 2.58xl0 - 3 4 Js
(b)
For an / state, Z = 3
L = [Z(/ +1)] 1/2 h = (12)1/2(1.055 x 10 - 3 4 Js) = 3.65 x KT 34 Js
55
56
CHAPTER 8
QUANTUM MECHANICS IN THREE DIMENSIONS
8-19
When the principal quantum number is n, the following values of / are possible:
/ = 0, 1, 2, ..., n - 2, n - 1 . For a given value of /, there are 21 +1 possible values of ml. The
maximum number of electrons that can be accommodated in the n * level is therefore:
(2(0) + l) + (2(l) + l) + ...+(2Z + l) + ...+(2(n-l) + l)=s2"f;/ + S / = 2"f;/ + n.
(=0
1=0
(=0
k
k(k + l)
But£Z = - i
so the maximum number of electrons to be accommodated is
;=o
2
2(n - \)n
2
—
—+n=n\
8-21
(a)
i
y 2 s (r):
r i ^3/2
4(2^)V2 V"o
2 - — |e" r/2a °. At r = a0 = 0.529 x 10"10 m we find
«0
\3/2
^2s(«o) =
2
4(2^-)V Uo
= (0.380)
(2 -l)e~ 1 / 2 =(0.380)f —
1
0.529 x l 0 _ 1 0 m
3/2
= 9.88xl0 14 m- 3 / 2
2
(b)
|^ 2s (fl 0 )| 2 =(9.88xl0 14 nT 3 / 2 ) =9.75xl0 2 9 m" 3
(c)
Using the result to part (b), we get P2s(flo) = 4;znol^2S(«o)|2 =3.43xl0 1 0 m" 1 .
(a)
—=
i
8-23
»
nc
r- =
k2
(e.esxio-^jsXsx^m/s)
5- =
2^(9xl0 9 Nm 2 /C 2 )(l.6xlO- 1 9 C) 2
(b)
-£•=
' e = - — = — = 2^x137
r0 ke*/mec*
far
a
(c)
a0 _ h2/meke2 _ 1 ftc _ 1 = 137
Ac
Ymcc
2 ^ t e 2 2;rar 2;r
m.fce2
(d)
8-25
fan
li/XjoO
Anch 3 \
: _ _ - = — = 4^(137)
\mek2ei j far
a
The most probable distance is the value of r which maximizes the radial probability density
P(r) = \rR(r)\2. Since P(r) is largest where rR(r) reaches its maximum, we look for the most
tHrR(r}}
probable distance by setting —
equal to zero, using the functions R(r) from Table 8.4.
x
For clarity, we measure distances in bohrs, so that — becomes simply r, etc. Then for the 2s
«o
state of hydrogen, the condition for a maximum is
0 = |-{(2r-r 2 )e- r / 2 } = { 2 - 2 r - i ( 2 r - r 2 ) l e - r / 2
MODERN PHYSICS
57
or0 = 4-6r + r 2 . There are two solutions, which may be found by completing the square to
get 0 = (r - 3)2 - 5 or r = 3 ± V5 bohrs. Of these r = 3 + V5 = 5.236a0 gives the largest value of
P(r), and so is the most probable distance. For the 2p state of hydrogen, a similar analysis
gives 0 =—{r2e~r'2} = \lr—r2
\e~rl2 with the obvious roots r = 0 (aminimum) and r = 4 (a
maximum). Thus, the most probable distance for the 2p state is r = 4a0,in agreement with the
simple Bohr model.
8-29
To find Ar we first compute (r2j using the radial probability density for the Is state of
hydrogen: Pls(r) = \r2e~2rl"<'. Then (r 2 ) = °jr2Pu (r)dr =a -|-Jr V 2r/fl °dr. With z a= —, this is
"o
0
oo
o
(r2) = — —
} z *e~zdz. The integral on the right is (see Example 8.9) JzV 2 dz = 4! so that
(r 2 ) = -i-f—1 (4!) = 3a2 and Ar = ((r 2 )-(r) 2 ) V2 =[3a^ -(1.5fl0)2]1/2 =0.866o0. Since Ar is an
a0 \ 2 J
appreciable fraction of the average distance, the whereabouts of the electron are largely
unknown in this case.
8-31
A
.
dU
A
Outside the surface, U(x) = — n(to
(togive
givecFF==——
——==—— j ) , and Schrodinger's equation is
x
ax
x
h2 ^ 2
—Y+1
W(x) = E \ff(x). From Equation 8.36 g(r) = rR(r) satisfies a one-dimensional
2m J
Schrodinger equation with effective potential U^ (r) = U(r)+
z—. With I = 0 (s states)
2m
r
e
kZe2
and LT(r) =
the equation for g(r) has the same form as that for y/(x). Furthermore,
y/(0) = 0 if no electrons can cross the surface, while g(0) = 0 since R(0) must be finite. It
follows that the functions g(r) and y/(x) are the same, and that the energies in the present
(Z2ke2 V 1 "\
case are the hydrogenic levels E„ =
—5- with the replacement kZe2 -» A.
{ 2aQ JKn'J
Remembering that a0 =
T, we get E„ - - — 5 - —T I n ~ I, 2, ...
meke2
yih2 jKn2 J
9
Atomic Structure
9-1
AE = 2juBB = hf
2(9.27 x 10 -24 J/T)(0.35 T) = (6.63 x 1CT34 Js)/ so / = 9.79 x 109 Hz
9-3
(a)
n = l;forn = l , / = 0 , m , = 0 , m s = ± —
1
1
->2sets
m,
0 - 1 / 2
0
+1/2
0
0
2n 2 = 2 ( l ) 2 = 2
(b)
For n = 2 we have
n
2
2
2
2
/
0
1
1
1
«i
0
-1
0
1
ms
±1/2
±1/2
±1/2
±1/2
Yields 8 sets; In = 2(2) = 8. Note that the number is twice the number of mt values.
Also that for each I there are 2/ +1 m, values. Finally, 1 can take on values ranging
n-l
from 0 to n -1, so the general expression is s = J] 2(2/ +1). The series is an arithmetic
o
progression: 2 + 6 + 10 + 14..., the sum of which is
s = — [2a + (n-l)d]
wherea = 2, d = 4
It
s = - [ 4 + (n-l)4]=2n 2
It
(c)
n = 3:
2(l) + 2(3) + 2(5) = 2 + 6 + 10 = 18 = 2n 2 = 2(3) 2 =18
(d)
n = 4:
2(1) + 2(3)+ 2(5)+ 2(7) = 32 = 2n2 =2(4) 2 =32
(e)
n = 5:
32 + 2(9) = 32 + 18 = 50 = 2n 2 =2(5) 2 =50
59
60
CHAPTER 9
ATOMIC STRUCTURE
9-5
The time of passage is t = —
1 m
— = 0.01 s. Since the field gradient is assumed uniform, so is
1
OH
the force, and hence the acceleration. Thus the deflection is d = —at2, or a = —?- for the
2
t2
acceleration. The required force is then
_ Mid _ 2(108 u)(l.66xl0- 27 kg/u)(lQ- 3 m)
F
Z
f2
(l0- 2 s) 2
The magnetic moment of the silver atom is due to a single unpaired electron spin, so
Thus,
dB,
dz
9-7
R
// z
3.59x10"^
= 0.387 T/m.
9.27 xlO - 2 4 N
The angular momentum L of a spinning ball is related to the angular velocity of rotation 00 as
L = la. I, the moment of inertia, is given in terms of the mass m and radius R of the ball as
I =—mR2. For the electron this gives
J = - ( 5 1 1 x l 0 3 e V / c 2 ) ( 3 x l 0 _ 6 n m ) 2 = 1.840x10"* e V n m 2 / c 2 .
Then, using L =—A, we find a = - = —
( 197 - 3 e V n n Y c )
=
6
2
7 2 1.840 xlO - 6 eVnm 2 /c 2
equatorial speed is
v = Ra) = (3xlO'6
9 - 2 8 6 x 1Q7 c / n m
The
'
nm)(9.286xl0 7 c/nm) = 278.6c
-=278.6
c
9-9
3
f [15]1/2 ^
With s =—, the spin magnitude is |S| = [s(s +1)] 1 ' 2 A =
m. The z-component of spin is
2
2 J
Sz = msft where ms ranges from -s to s in integer steps or, in this case,
3
1 1 3
ms=—, — , +—, + —. The spin vector S is inclined to the z-axis by an angle 0 such that
Zk
Zt
...
S,
|S|
JJ
Zt
msh
, ,
([15]V' 2/2)A
COS(g) = - £ - = ,
=
m,
3
1
1
' , 2 , = - • — H T 1T 2/ -TT—ITT-'
1/2 +T7Z7r7T'
12
[15]V /2
(15) / ' (15) ' (15) / '
r
3
(15)1/2
+"
or (9= 140.8°, 105.0°, 75.0°, 39.2°. The Q.~ does obey the Pauli Exclusion Principle, since the
spin s of this particle is half-integral, as it is for all fermions.
MODERN PHYSICS
9-11
1
1 1
For a d electron, Z = 2; s = - ; ;' = 2 + - , 2 —
J
2
2
2
3 _1_ 1_ 3 5
For;=|;m;.=-|
V
2'2'2'2
For;=|;m;.=-|,
9-13
I I 3
2'2'2
(a)
4 % -*n = 4,l = 3,j = -
(b)
in-w/+D^-[(IXfF»=
35' 1/2
(35)V2
h=
4.
/ z = m;-ft where m ; can be - / , -j + 1,..., j - 1 , j so here m;- can be
1
3
5
5
3
X
3
5
_5 _3
! —,
* —
f«
e , !—
f c h, *
c n.
—, —,
—. /J7 can ube — *n , -—ft,
—n, or f—
z
2' 2
2 2 2 2
2
2
2 2 2
2
(c)
9-15
61
The spin of the atomic electron has a magnetic energy in the field of the orbital moment given
by Equations 9.6 and 9.12 with a g-factor of 2, or IT = -\LS • B = 2
\SZB = 2^iBmsB. The
magnetic field B originates with the orbiting electron. To estimate B, we adopt the equivalent
viewpoint of the atomic nucleus (proton) circling the electron, and borrow a result from
classical electromagnetism for the B field at the center of a circular current loop with radius r:
B - —Y~ . Here km is the magnetic constant and // = inr1 is the magnetic moment of the
loop, assuming it carries a current;'. In the atomic case, we identify r with the orbit radius and
the current i with the proton charge +e divided by the orbital period T =
evr
2KT
. Then
L where L = mevr is the orbital angular momentum of the electron. For a p
2me) J
electron/ = 1 and L = [/a + l)]1/2n = V2A, s o / / = [ —
|V2 =// B V2=1.31xlO - 2 3 J/T.Forrwe
take a typical atomic dimension, say 4a 0 (= 2.12 x 10 ~10 m) for a 2p electron, and find
2(l(T7 N/A 2 )(l.31xl0 - 2 3 J/T)
B=—
^
= —- = 0.276 T.
(2.12x10 "10 m) 3
Since ms is ±— the magnetic energy of the electron spin in this field is
U = ±nBB = ±(9.27 x 10 -24 J/T)(0.276 T) = ±2.56 x 10 -24 J = ±1.59 x 10"5 eV.
The up spin orientation (+) has the higher energy; the predicted energy difference between
the up (+) and down (-) spin orientations is twice this figure, or about 3.18 x 10~5 eV —a
result which compares favorably with the measured value, 5 x 10 ~5 eV.
62
CHAPTER 9
ATOMIC STRUCTURE
(h2n2
9-17
From Equation 8.9 we have £ =
\
j
{n\+n\+n2)
\2tnL J
E
(a)
=-
:
'
'2
2(9.11 xl0- 3 1 )(2xl0 - 1 0 )
j
= 1-5x10-" J )(n2+n2+n2
)=
(9AeV)(n2+n2+n2)
2 electrons per state. The lowest states have
(n2 +n\ + n 2 ) = (l, 1, l ) = > E m =(9.4 eV)(l 2 + 1 2 +1 2 ) eV = 28.2 eV.
For(n 2 +w 2 +n 3 2 ) = (l, 1, 2) or (1, 2, 1) or (2,1,1),
£112 = Em= Em= (9.4 e V ) ( l 2 + l 2 + 2 2 ) = 56.4 eV
Emin=2x ( E m + E m + E m + £ 211 ) = 2(28.2 + 3 x 56.4) = 398.4 eV
(b)
All 8 particles go into the (n2 +nl+n2) = (1, 1, 1) state, so
£ m i n = 8 x £ m =225.6 eV.
9-21
(a)
ls 2 2s 2 2p 4
(b)
For the two Is electrons, n = l,
Z = 0, ml = 0 , ms =±—.
For the two 2s electrons, n = 2, Z = 0, m, = 0, ms = ±—.
9-23
For the four 2p electrons, n = 2, Z = l , m, = 1 , 0, - 1 , ms =±—.
z
All spins are paired for [Kr]4d10 and two are unpaired for [Kr]4d95s1. Thus Hund's rule
would favor the latter, but for the fact that completely filled subshells are especially stable.
Thus [Kr]4d10 with its completely filled 4d subshell has the lesser energy. The element is
palladium (Pd).
9-25
A typical ionization energy is 8 eV. For internal energy to ionize most of the atoms would
3
2 x 8(1.60 xl(T 1 9 J)
require
-fc
T
=
8
eV:
T
=
^—-i
=
~T~ between 104 K and 105 K.
B
n
2
3(1.38 xlO' 2 3 J/K)
9-27
(a)
The L a photon can be thought of as arising from the n = 3 to n = 2 transition in a oneelectron atom with an effective nuclear charge. The M electron making the transition
is shielded by the remaining L shell electrons (5) and the innermost K shell electrons
(2), leaving an effective nuclear charge of Z - 7. Thus, the energy of the L a photon
u u u rfT 1 te2 (Z-7)2
ke2 (Z-7)2
ke2 5(Z-7) 2 ... _
_ ,,
.
should be £[L B ] = —
-5—+—
^ + i r - - L 1 - ^ . W n t i n g £ = ^/and
2a0
3
2a0
2
2aQ
36
ke2
noting that
= 13.6 eV this relation may be solved for the photon frequency/.
2a0
Taking the square root of the resulting equation gives -ff = J—(—'•
\{Z-7).
MODERN PHYSICS
(b)
63
According to part (a), the plot of 7 7 against Z should have intercept = 7 and slope
l±(*i*L)
V36l
h
J
8
1 2
= j . 5 ( 1 3 - 6 e1P5
9.18 we find
x" = 0.214xl0 Hz / . From Figure
6
y 36(4.14 xl(T eVs)
data points on the La line [in the form (77/ Z)] a t (14,74) and (8,45). From this we
14 — 8
obtain the slope
= 0.21 x 108 Hz V 2 . Thus, the empirical line fitting the La data
is 7 7 = 0-21(Z - 1 ) where I is the intercept. Using (14,74) for ( 7 / , Z) in this equation
gives the intercept 1 = 7.3, but with (8,45) for (77/ Z) we get I = 6.9. Alternatively,
using both data pairs and dividing, we eliminate the calculated value of the slope to
14 74-7
get — =
. This last approach affords the best experimental value for I based on
the available data and gives
I = ( 1 4 ) ( 4 5 ) " ( 8 ) ( 7 4 ) = 6.3.
6
14-8
(c)
The average screened nuclear charge seen by the M shell electron is just
Z - 7 = Z - 6.3, indicating that shielding by the inner shell electrons is not quite as
effective as our naive screening arguments would suggest.
10
Statistical Physics
10-1
Using tij =n;1/7j +tij2p2 +••• we obtain:
" l = " l l P l +«12P2 +"120P20 = ( ° )
1287
+ a/^) + (o{ T | 7 ) t (2{ T ^l +( o{
1287,
1287.
1287
»
V 1287J
( 15
60
180
120
60
120
_30_
+ (3)
+ (0)
+ (4)
+ (2)
+ (D
+ (0)
1287
1287
1287.
1287
J
1287
U287,
1287;
90 "j
120
60
180
+ (2)
+(0)
+ (3)
+ (5)
+ (D
1287 J
1287
1287
\l287j
\1287)
1287
1287 J
/ 15
+(4)
1287,
30 + 120 + 120 + 180 + 120 + 360 + 120 + 180 + 180 + 360 + 30 + 120 + 60
1287
= 1.538 46
+(D
py ( 1 £ )= a = l^3l= 0.256.
6
6
One can find p(2E) through p(8£) in similar fashion.
10-3
A molecule moving with speed v takes — seconds to cross the cylinder, where d is the
v
cylinder's diameter. In this time the detector rotates ^radians where 0= cot =
. This
v
d
cod2
means the molecule strikes the curved glass plate at a distance from A of s =—0 =
as
K
^
2
2v
mBi2 = 6.94xl0 _ 2 2 g and
(v) =
8kBT
1/2
(8)(l.38xl0 -23 J/K)(850K)
(^)(6.94xl0 _25 kg)
3kBT^2
= 207 m/s
f2kr,T\V2
= 225 m/s
ump= —2-J
m
6250x2^-^ (0.10 m) 2
= 1.45 cm
60s ;(2)(225) m/s
S(„) = 1.58 cm
s mp = 1.78 cm
65
=184 m/s
66
CHAPTER 10
STATISTICAL PHYSICS
10-5
Fit a curve Ae~BE to Figure 10.2. An ambitious solution would use a least squares fit to
determine A and B. The quick fit suggested below uses a match only at 0 and IE. P(E) = Ae~m
thus P(0) = A and P{E1) = Ae~BBl . From Figure 10.2 one finds P(0) = 0.385 , and this gives
A = 0.385. To determine B use the value P(1E) = 0.256 = AT BE ' = 0.385e-B£' thus e_BE' = 0.665
and B =
- l n ( a 6 6 5 > = .9J08 a n d so P(E) = (0.385)<r(a408E/£>>. This equation was used to
E1
E1
determine the probability as follows P(0) = 0.385, P(1E1) = 0.256, P(2Et ) = 0.170,
P{3El) = 0.113, P(4E!) = 0.075, P(5Ea ) = 0.050, P(6E: ) = 0.033, P(7Ej ) = 0.022, P(8Et ) = 0.015 .
The exact values are P(0) = 0.385, P(lEj ) = 0.256, P(2Ea ) = 0.167, P(3EX ) = 0.078,
P(4Ej) = 0.054, P{5El) = 0.027, P(6Ej) = 0.012, P{7EX) = 0.003 9, P(8Ea) = 0.000 717. These
values are plotted below. One sees that this approximation is good for low energy. There is
exact agreement for P(0) and P(1E) and small deviations for the next two values with
percent deviations for the higher energy values.
0)
T3
•J3
A3
(JO
M
OJ
c c
••B
a
m C
a
•8
Energy
10-7
(a)
Ev
=-pe=-ecos0°=-pe
ED = - p £ , = -fcosl80°=+p£
so AE = ED - Ev = 2pe.
(b)
Let n(2pe) be the number of molecules in the excited state.
n(2pe) g{2pe)Ae-2ps/k<>T
•n(0)
g{0)Aeu
2e~2velk*T
MODERN PHYSICS
(c)
L90 = n(2p£) = 2 e . 2 p £ A B T
1
n(0)
por
r
10xlo-3o C m a n d e =
(L0xl06
\
67
)
I )'
v/m
2pe _ (2)(1.0 x 10"30 Cm)(l.O x 106 V/m) _ 0.144 9
(1.38 xlO" 23 J/K)T
T^f~
T
so 1.90 = 2e-° 1449/T or 0.95 = e~°Mi9'T. Solving for T, ln(0.95) = ^ ^ 1
W
L V H m
H J
n(2pf)+n(0)
orT
= 2.83 K .
2e- 2 f , ^" T +l
[n(2p*)+n(0)][n(2pf)+n(0)]+l
2pe
l + a^e2^"7"
As T - > 0 , £ - > 0 and as T->°°, E->
(e)
d
c
Etotal=NE =
2pe
3/2
fye
3
2p£W
l + (l/2)e2p£/'tBT
_ d£ tota , _ ( M B / 2 ) ( 2 p g / f c B r ) V ^ r
dT
[l + (V2)e2'"/*»r]
2iV£
(£)
By expanding e* where x = ——
fcBT one can show that C —»0 for T -> °° as
2A
c.r^)V*
V "-B y
1
T*
-) and C -> 0 for T -> 0 as C -
maximum in C = I —r^- \(x2)
„.. ,,
derivatives we get:
(2M
/
e
(1 + 0/2)**)
• To find the
\
dC n
fdCYdx)
=4 set — = 0or — — =0. Taking
2 / '[[i+a/^fj
-xV
* }^pe/k
f e fB/T f r ^
^
UJUT-J
2 + x-xex
_l + (l/2)e*
Setting the first factor equal to 0 yields the minima in C at T = 0 and T = °°, while the
second factor yields a maximum at the solution of the transcendental equation,
x + 2 ex
= — . This transcendental equation has a solution at x ~ 2.65, which
x-2
2
, 2pe „ ,_
rr,
2pf
0.1449 „ „ _ „ „ „ , „,,
corresponds to a temperature of ——
._. = 2.65 = 0.054 7 K. The
fc T = 2.65 or T = 2.65fc
B
B
expression for heat capacity can be rewritten as C = A
where
(l + ( l / 2 K )
l L .and
n ^x =, —£—.
M Below is the sketch of C as a function of 2pe
A -= ——
2
k BT
k BT
68
CHAPTER 10
STATISTICAL PHYSICS
NkB/2
2pe
The heat capacity is the change of internal energy with temperature. For both large
temperature (T —* °°) and low temperature (T -> 0) the internal energy is constant
and so the heat capacity is zero. At T approximately equal to 0.0547 K there is a rapid
change of energy with temperature; so the heat capacity becomes large and reaches
its maximum value.
10-9
v=
8knT
Using a molar weight of 55.85 g for iron gives the mass of an iron atom:
nm
5585 g
,,
(8)(1.38x 10 -23 J/K)(6000 K)
,
26
m=
=9.28xl0- kg. Thus, v=J-^
' JV x
- = 1 . 5 1 x l 0 3 m/s.
;
6.02X1023
\
(^)(9.28xl0 _26 kg)
Since the speed of the emitting atoms is much less than c, we use the classical doppler shift,
/ = / 0 (l±p/c).Then
33 83g
Af „ /ma, -/^ax „ /„(! +P/C)-/„(!-i>/c) = 2v
/o
/o
/o
=
(2)(l.51xl0 3 m/s) _
c
3.00xl0
8
i m
^
Q
_
m/s
or 1 part per 100 000,
10-11
12E
5£(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
5
MODERN PHYSICS
Thus,
1
1
1
1
1
1
1
1
1
n 00££ = - x 2 + - x 2 + - x 2 + - x 2 + - x 2 + - x 2 + - x 2 + - x 2 + - x 2 = 2.00
9
9
9
9
9
9
9
9
9
n 0£ through n5E = 2.00
n 6 E = 8 ( i x 2 ) + ( i x l ) = 1.89
^£=7(Ix2)+(Ixl)+(Ixl)
n8£=6(ix2]+(ixl]
+
=
1.78
( i x l ) = 1.55
n 9E = 4 ( | x 2 ) + ( i x l ) + ( I x l ) + ( I x l ) = 1.22
^ - ( ^ l )
+
«nE=gx2)
g x l )
+
( I x l ) + ( I x 2 ) + ( I x 2 ) = 0.777
gxl)
+
1.444
( i x l ) = 0.4
+
"i2E = f - x l l + f 4 x l ) = 0.222
» i 3 E = ( | x l ) = 0-111
n 14E =0.00
Minimum energy occurs for all levels filled up to 9E, corresponding to a total energy of 90E.
So EF (0 K) = 9E. Using Equation 10.2 the following plot is obtained.
0
j
i
i
1--..1
1 2 3 4 5 6 7 8 9 10 11 12 13 14 Energy
States
»<2>/Jc B T E
10-13
(a)
hco
C = (3R)
-.ForT = TE, fcBrE=Aflj,so
W E J (e^Bi-E.!)'
fftaA 2
C = (3K)
ha/no)
• = (32?)——r = (32?)(0.920 7) = 2.762?.
Using 2? = 1.986 cal/mol K => C = 5.48 cal/mol K.
(b)
From Figure 10.9, TE lead = 100 K, TE aluminum » 300 K, TE silicon = 500 K.
69
70
CHAPTER 10
(c)
STATISTICAL PHYSICS
Using C = ( 3 R ) ^ j
e
T Jr
= (5.97 cal/mol K ) ( - M - ) eT*'T heat capacities for
lead, aluminum, and silicon were obtained. These results can be summarized in the
following tables.
T E =100K
Lead
T(K)
C(cal/(mol K))
4.32
5.49
5.74
5.83
T E =300K
C(cal/(molK))
0.535
2.96
4.32
4.97
TE-500K
C(cal/(mol K))
0.027
1.02
2.55
3.64
4.97
4.76
5.05
5.25
5.41
5.50
5.59
50
100
150
200
Aluminum
T(K)
50
100
150
200
Silicon
T(K)
50
100
150
200
250
300
350
400
450
500
550
T(K)
250
300
350
400
T(K)
250
300
350
400
T(K)
600
650
700
750
800
850
900
950
1000
1050
1100
C(cal/(molK))
5.92
5.94
5.96
6.09
C(cal/(molK))
5.30
5.509
5.62
5.70
C(cal/(mol K))
5.64
5.67
5.74
5.75
5.78
5.81
5.84
5.85
5.83
5.85
5.95
These values are now plotted on Figure 10.9 as shown.
7
6
£
o
4
400
600
800
Absolute temperature, K
1000
1200
MODERN PHYSICS
10-15
A1:EF =11.63 eV
(a)
EF
3 V h2 J
2me \.Bx)
so
-31
_19
J/eV)
8n (2)(9.11xl0 kg)(11.63eV)(l.6xlO
3/2
= 1.80xl0 29 free electrons/m 3
(6.625 xlO" 34 Js)
pH
(b)
10-17
71
(2.7 g/cm 3 )(6.02xl0 23 atoms/mole)
n =
M
27 g/mole
n' = 6.02xl0 22 atoms/cm 3 = 6.02xlO28 atoms/m 3
n 18X1028 „
Valence = — =
=s- = 3
n'
6x10 28
/ t M _3N_ 2/3
N
. Substituting the mass of a
Equation 10.46 gives EF(0) in terms of — as EF =
v 2 m , 8/rFj
proton, and noting that A = 64 for Zn, m = 1.67 x 10-27z / kg; N =—=32 and
z*
V = -xR3 =-(^)(4.8xl0 - 1 5 m) 3 = 4.6xl0 - 4 3 m 3 yields
_(6.62xl0" 3 4 ) 2 J 2 s 2
U
_
f
^
27
3.34xlO""
kg
,2/3
(3)(32)
( 8 ^ 4 6 x 1 0 " ° m3)
= 5.3x10"" J = 33.4 MeV
Eav=|EF=20MeV
These energies are of the correct order of magnitude for nuclear particles.
10-19
/ FD =[e<E-E»>/*»T +l] _ 1 ; EF =7.05 eV;fcBT= (1.38 x 10 -23 J/K)(300 K) = 4.14x 10 -21 J = 0.0259 eV
At E = 0.99EF, / F D =[e-ooiEF/kBr + 1 j - J
=
e -0.0705/0.0259 + 1
L0
6 5 70
= 0.938, thus 93.8%
probability.
10-21
p = 0.971 g/cm 3 , M = 23.0 g/mole (sodium)
(a)
NAP
n = -M
n = (6.02xl0 23 electrons/mole)(0.971 g/cm 3 )(23.0 g/mole)
n = 2.54xlO 22 electrons/cm 3 =2.54xlO 28 electrons/m 3
(b)
EF=^r^f
2mV8^7
£F =
(6.625xlO""34 Js)
(2x9.11 xlO" 31 kg)
19
E F = 5.04 xl0 _ 1 M = 3.15 eV
3x2.54xlO 28 electrons/m 3
2/3
72
CHAPTER 10
STATISTICAL PHYSICS
« -i'^r-
2x5.04xl0"" 19 J
9.11xl0- 31 kg
-11/2
i> F =1.05xl0 6 m/s
10-23 rf = 1 mm = 10"3 m; V = (lO"3 m) = 10' 9 m 3
The density of states = g(E) = CE1'2 = j
8
^ ^ " ^
W
,« /
,1 , 3 / 2 f(4.0eV)(l.6xlO- 19 J/eV)l
31
;J
£(E) = 8(2)V^9.11xlO- kg 3 / 2 ^
-^
3
34
(6.626 xKT Js)
1/2
^•(E) = (8.50xl0 46 )m -3 J -1 =(l.36xl0 2 8 )m' 3 eV _1
/FD(£)= e ( £ _ £ F ) A B r + 1 or
/FD(40 eV) =
•/^UV
^
\
;
= —=J— = 1
(4.0-5.5)/(8.6xl0- 5 eV/K)(300 K)
..
+1
e
So the total number of electrons = N = g(E)(A£)V/FD(£) or
N = (l.36xl0 2 8 m - 3 eV_1)(0.025 eV)(lO-9 m 3 )(l) = 3.40xl0 17 .
10-25
Use the equation n{v) = —
H
V-
2
21 T
5?rz> e~''"' " B )
3/2
where m is the mass of the O , molecule
(2xkBT)
in kg and — is 104 molecules per cm 3 . Rewrite the equation in the form
n(v) = AA—-J
u2e~/l31' where A^ =
, A2 =
,andA3=
. Use the exponential
format for large and small numbers to avoid computer errors.
(a)
For T = 300 K the equation can be rewritten as n(v) = B1v2e~BlV where
(A \3^2
A
B1 = AA —2-1 and B2 = —^-. Do a 21 step loop for v from 0 to 2 000 m/s storing
n300(0 as an array where i = 1 to 21 and corresponds to u = 0 to 2 000.
(b)
Repeat the calculation in (a) except that the A's are now divided by 1 000 and call the
array nl000(;') where ;' = 1 to 21 and corresponds to v = 0 to 2 000.
(c)
Use a plot routine to obtain a graph similar to Figure 10.4 for the arrays obtained in
parts (a) and (b). To obtain the number of molecules with speeds between 800 m/s
and 1 000 m/s do a summation. The number of molecules
= [nl 000(9)](100) + [nl 000(10)](100) where nl 000(9) and nl 000(10) is the number
calculated in (b) for speed 800 m/s and 900 m/s, respectively.
f3fcBry/2
(d)
r8ArBrV/2
vms = — — I ; uav = — —
f2itBry/2
TU
..
...
; i>mp = — — I . These quantities should appear
on your graph as shown in Figure 10.4.
MODERN PHYSICS
10-27
(a)
Forametalg(E) =
8(2)V2 nml/2
EV^DEV* where D J ^
m
l
73
/ 2
3
and
h
2
15
me = 0.511 MeV/c and h = 4.136 x 10" eV s. Using a loop calculate the array g(E)
for values of energy ranging from zero to 10 eV in steps of 0.5 eV. The array will be
21 dimensional, which can be plotted using a plot routine.
(b)
h2 f 3N ^3
EF(0) = -2— -^—
= 7.05 eV from Table 10.1. For T = 0 and EF < E
2me {8srV J
f
1
1
0
«(£) = 0.
ForT = 0 and EF =E, n(E) = [ —jEp^.For 1 = 0 a n d 0 < E < E F one has
/PD =
= 1. Therefore n(E) = ^(E) where g(E) is obtained from the array
e~~° +1
calculated in part (a). Use the same 0.5 eV steps in your loop.
(c)
n(E) = ^(E)/ FD (E)
Now calculate fm = , r c w. _
where T = 1000 K in intervals of 0.5 eV for
e *>'k*'+1
E = 0 eV to 10 eV. EF is determined for any temperature T numerically using the
electron concentration
^ln(E)dE
=
Dle_{EEEf)Z+1kBT
that is of the order of 10"20. The dependence of EF on temperature is weak for metals
and will not differ much from its value at 0 K up to several thousand kelvin and
E-EF
E - EF should be less than 10, which means
is large. Thus
KBT
hi
°°
V
o
— = D f E^2e{E~ET)kBTdE. This can now be evaluated numerically. Once EF is
determined then the Fermi Dirac distribution function, / FD = , r c ...
, can be
e* F '' B +1
evaluated as an array using the same energy increments as before. The particle
distribution function, n(E), is the product of the arrays g(E) and / F D (E). Now n(E)
can be plotted as a function of energy.
11
Molecular Structure
11-1
(a)
We add the reactions K + 4.34 eV -> K+ + e" and I + e" -> I" + 3.06 eV to obtain
K +1 -> K+ + T + (4.34 - 3.06) eV. The activation energy is 1.28 eV.
(b)
dU 4€
™
= *±
dr
a
-«£W^''
At r = rn we have
' a)
dU
O.Here
dr '
vo/
If a 1
2 U'OS
= 2-V«,
a = 2"V6 (0.305) nm = 0.272 nm = (T
Then also
U(r0) = 46
r2"V 6 r n
V
12
'0
r2-V«r„Y
V
'0
S
+ £,
= 4e[I-I
+ E„=-e+E„
L4 2
e = E8 - U(r0 ) = 1.28 eV +3.37 eV = 4.65 eV
r
(c)
?(/)=-—=—
ar
cr
/^-\13
-<ffj
-]
To find the maximum force we calculate — = —r- -1561-1
+42f-l
dr a
a
r
rupture
=0when
( 42 V/ 6
U56J
1(4.65 eV)
=L
0.272 nm
U56;
U56J
'max
19
1.6xlQ- Nm
= -6.55nN
:-41.0
10 -9 m
F
= -41.0 eV/nm
Therefore the applied force required to rupture the molecule is +6.55 nN away
from the center.
/
75
76
CHAPTER 11
MOLECULAR STRUCTURE
11-3
For the / = 1 to / = 2 transition, AE = hf-
[2(2 + l ) - l ( l + l)]ft2
2n
or hf =
. Solving for / gives
21
6.626 xlO -34 J s
1 = in
,, , -/
,w
11 . - 1 . 4 6 x l O - " kg m z ; / / = — i - A - = 1.14x10"* kg,
1
2
5
&
hf
2K f (2/r )(2.30xlO n Hz)
m1+m2
\V2
= 0.113 nm, same as Example 11.1.
Rn
f*2\
11-5
(a)
The separation between two adjacent rotationally levels is given by A£ =
I )
where / is the quantum number of the higher level. Therefore
AE,
^65
AE-10
l
10 '
J1
6A65 = 6(1.35 cm) = 8.10 cm
c
Aw
°
=
^10
3.00x10cm/s
8.10 cm
Hz
AE10 -hf10 —r'>
(b)
1=
2/rfw
1.055 x l O - * J s
(2^-)(3.70xl0 9 Hz)
7 = 4.53xl0"45kgm2
(h2\
11-7
HCI molecule in the I = 1 rotational energy level: R0 = 1.275 A, Erot = — /(/ +1). For I = 1,
\2I J
'2h^V1
h2
la2
•,a =
ttoi
~ I ~ 2
I2
-'TH
/=
(1 u)(35 u)
1"'2
m,m
Rl = [0.972 2 u x 1.66 x 10"27 kg/u] x (1.275 x 10"10 m) 2
RZ =
. 1u + 35u.
m1 +m2
= 2.62xl0" 4/ k g m
34
Therefore, a=\ — \Jl =
iw
^_m_
mi+ff^
=
1.055 x l 0 _ J 4 J s
2.62 xlO - 4 7 k g m
V2=5.69xl0 1 2 rad/s.
auK35u) = r35^ u = L 6 2 x l 0 - 2 7
(lu + 35u) \36J
k
&
MODERN PHYSICS
(a)
/ = pR2 = (1.62 x 10 -27 kg)(l.28 x 10"10 m) 2 = 2.65 x 10 -47 kg • m 2
cF
-
rot
21
h2 _
W + l)
(1.054 x 10 -34 J s) 2
2.1 xlO _ z z J = 1.31x10^ eV
27~2x2.65xl0-47kgm2
E r o t =(l.31xlO - 3 eV)/(/+l)
£rot=0
E r o t =2.62xHT 3 eV
E r o t =7.86xlO _ 3 eV
E rot =1.57xKT 2 eV
1=0
1=1
1=2
1=3
(b)
17:
Kx'
,U = 0.15 eV when x = 0.01 nm
(0.15eV)(l.6xHT 19 J/eV)
K(W-n m)2
K = 480 N/m
/ =
(c)
UK)1/Z
2K\H
_ j_
2K
1/2
480
-27
L 1.62x10
= 8.66xl0 13 Hz
Eva,=l»+2>F
ft/ = (6.63 x 10~34 J s)(8.66 x 1013 Hz) = 5.74 x 10' 20 J = 0.359 eV
E0 _M._oc7^m-20
= -f- = 2.87 x 10_zu J = 0.179 eV
2
KA2
2.87X10- J = M i » l
E=
2p\l/2
—
= 1.09 x 10 -11 m = 0.109A = 0.010 9 nm
KJ
El=-hf
AJ
(d)
he
=
AE
= 8.61 x 10_zu J = 0.538 eV
=I — J
= 1.89 x 10 -11 m = 0.189 A = 0.018 9nm
min ° r ^max =
he
AE„
Rotational
AE m i n =E / = 1 -E, = 0 =2.62xlO- 3 eV
/tc = 12 400eV-A
12 400
= 4.73 x 106 A = 4.73 x 10"4 m (microwave range).
7
—2.62x10"
77
78
CHAPTER 11
MOLECULAR STRUCTURE
Vibrational
he _ c _3.00xlQ 8 m/s
he
: 3.46 x 10
AE
min ~ ¥ ~ / ~ 8.66xl0 13 Hz
11-11
The angular momentum of this system is L ••
mvRn
+
mvR,
nh
L must be a multiple of h, L = mvR0 = nh, or v
m = 3.46 /an (infrared range).
= mvR0. According to Bohr theory,
with n = l, 2, .... The energy of rotation
mR0
is then
V
1
2
1
nh
m
R0,
v
2
nW
tnRl
n = l,2,
From Equation 11.5 the allowed energies of rotation are
2/„
-{/(/ + !)},
1 = 0,1,2,...
where I^, is the moment of inertia about the center of mass. In the present case, we have
,R0\2
(R0\2
2
mRZ
~
Thus,
mR;
1 = 0,1,2,
- W + l)}
We see that 1(1 + 1) replaces n2 in the Bohr result. The two are indistinguishable for large
quantum numbers (Correspondence Principle), but disagree markedly when n (or I) is small.
In particular, £ rot can be zero according to Quantum Mechanics, while the minimum
rotational energy in the Bohr theory is
11-13
-=- for n = 1.
mR2
At equilibrium separation R, Ueli is a minimum: 0 = — — = / / ^ ( R , - R 0 ) dr Ri
R - R
, l<! +
1
»
(
i
Kl + lW
MR3
or
\
. For I«—2-JL^ the second term on the right represents a small
Rf)
correction, and may be approximated by substituting for R its approximate value RQ to get the
l{l + l)h2_(l_}
next approximation R; ~ R0 + 2 2
The value of UeS at Rt is the energy offset U0:
M co 0
v ftRloy
RI-RQ+—2~2T
l(l + l)h2
M2a)20Rf
l(l + l)h2
2 MR 2o
l(l + l)h2
2MRf
l(l + l)h2
2M
Rf
l{l + l)h2
,,2,.„2p4
+1
MODERN PHYSICS
79
The curvature at the n e w equilibrium point is
d2Uelf
2
dr*
•-JUC0O+-
31(1+ 1W
MRf
and is identified with /ia\ to get the corrected oscillator frequency
^=^+M+l)*i.fflg
M2Rf
+
a
3W+i)*
2
H Kt
Since the second term on the right is small by assumption, ax differs little from a0, so that we
may write a2 - a2 = {wl - co0)(o)i + a0)~ 2CO0ACO. The fractional change in frequency is then
Aco
l)h2
2
2fi (o2R0i
a0
11-15
31(1+
The Morse levels are given by £ vib = v + — \ha-\ v+—\
. The excitation energy from
level v to level v +1 is
(ha)2
4U0
2
-ha~<\ v +
l)
V+
\\ \(ha)
2
r
ha l - ( u + l)
[ 2) J 4LZ0
ha^
y2U0JJ
It is clear from this expression that AEvib diminishes steadily as v increases. The excitation
energy could never be negative, however, so that v must not exceed the value that makes
ha , _
2U
-(v + 1) or u m , v - 0 — 1. With this value for v, the vibrational energy is
A£vib vanish: 1 =
2U0
"^
ha
J
1
[2U0-(l/2)ha]
vib = 2 L 7 n — h a
4U„
2
•un-
(fiaf
16LZn
2LZ
If — - is not an integer, then vmax a n d the corresponding £ v i b will be somewhat smaller t h a n
ha
the values given. However, the maximum vibrational energy will never exceed U0
.
16U0
11-19
To the left and right of the barrier site y/is the waveform of a free particle with wavenumber
y/(x) = A sin(fcx) + B cos(fcr)
0<x<-
y/(x) = F sin(foc)+G cos(fcc)
-<x<L
2
2
80
CHAPTER 11
MOLECULAR STRUCTURE
The infinite walls at the edges of the well require y/iff) = y ( i ) = 0, or B = 0 and G = - F tan(fcL)
leaving
0<x<-
y/(x) = Asin(kx)
2
y/(x) = F{sin(fcc)-tan(JtL)cos(fcc)}= C sin(for - JtL) -<,x<,L
A
For waves antisymmetric about the midpoint of the well, y/1 — = 0 and the delta barrier is
ineffective: the slope —— is continuous at —, leading to C = +A. For this case — -nn, and
2
2+ 2
n n h
2m(L/2)2
L
as befits an infinite well of width
n = l,2,...
3^2
The remaining stationary states are waves symmetric about —, and require C = -A for
Li
continuity of yr. Their energies are found by applying the slope condition with C = -A to get
2h2
AV fkL—
^ -J4A:COS
AU W— = (2mS
^A LAsin
• f fc
Y ^—M . Solutions
o . „
l lU-Akcos
—=—M or .tan W
— =-(
to
this
z
K2J
\2)
\h
r
\2)
\2)
, {mSLJ^ 2 J
equation may be found graphically as the intersections of the curve y = tanx with the line
2hA
y = -ax having slope -a -(see the Figure above). From the points of intersection x„
mSL
2x
hzk 2
we find kn - —i-5- and En = '*" . Only values of xn greater than zero need be considered,
L
2m
since the wave function is unchanged when k is replaced by -k, and k = 0 leads to y/(x) = 0
2
everywhere. As S -> °° we see that x„ - » n n , giving E„ = nV*
for S -» oo and n = 1, 2,
2m(I/2)
the same energies found for the antisymmetric waves considered previously. Thus, in this
limit the energy levels all are doubly degenerate. As S -»0 the roots become
2 2*2
K 3n
nn
. .
x„=~, — , . . . = — ( n odd), giving E„ - n n h n = 1, 3, ... . These are the energies for the
2 2
2
2mL
symmetric waves of the infinite well with no barrier, as expected for S = 0.
MODERN PHYSICS
81
The ground state wave is symmetric about —, and is described by the root xt, which varies
It
anywhere between — and ^"according to S. The ground state energy is
I*
_
t i1 —
h2(2Xl/L)2
2m
2x2h2
ml2
The first excited state wave is antisymmetric, with energy
K2%2 _ ITCH2
E,2
' ~2m(L/2)2~
ml2 '
which coincides with Ej in the limit S —> °°.
11-21
By trial and error, we discover that the choice R = 1.44 (bohr) minimizes the expression for
E tot , so that this is the equilibrium separation R0.
The effective spring constant K is the curvature of Etot W evaluated at the equilibrium point
K0 = 1.44. Using the given approximation to the second derivative with an increment
AR = 0.01, we find
2
c
fc _ "d F
tot
dR2
= 1.03.
(An increment ten times as large changes the result by less than one unit in the last decimal
place.) This value for K is in (Ry/bohr 2 ). The conversion to SI units is accomplished with the
help of the relations 1 Ry = 13.6 eV = 2.176 x 10"18 J, and 1 bohr = 0.529 A = 5.29 x 10"11 m.
Then K = 1.03 Ry/bohr 2 = 801 j / m 2 = 801 N/m. The result is larger than the experimental
value because our neglect of electron-electron repulsion leads to a potential well much deeper
than the actual one, producing a larger curvature.
12
The Solid State
12-1
U.Total
' ^attractive '
u
oke2
repulsive
eke2
dU.Total
dr
--Q = +
mB
„m+l
B .
.... .
, . . . ' ,
+ — • At equilibrium, U T o t a l reaches its m i n i m u m value.
. Calling the equilibrium separation r 0 , w e m a y solve for B
oke2
mB
„m+l
B=
eke*
mro"1-1
Substituting into t h e expression for LTTotal w e find
_
eke2
{cke2lm)r^
f
eke2^
\
'o J
m
,2"\
12-3
l7 = -ofc
m
'o;
U = -(1.747 6)(9xl0 9 Nm 2 /C 2 )
(1.6 xlO" 19 C) 2
0.281 x l 0 - 9 m
U = -1.25 x 10"18 J = -7.84 eV. The ionic cohesive energy is LT = 7.84 eV/Na + -OT pair.
,„12-5
7r
ke2
ke2
U=
r
r
u ..^
^
b u t l n ( l + x) = x
12-7
(a)
ke2
+
\U0
ke2
+
ke2
ke2
ke2
+
ke2
+
2r
x2
...=-2k
U2^ ,
1 1 1
1—+
+ ..
2 3 4
2r
2>r 3r
\r
4r
x3 xi
..
(21n2)te 2
+
+ . . . soLZ = —
—.
2
3
4
r
(1.747 6)(9.CX)xl09 N m 2 / C 2 ) ( l . 6 0 x H r 1 9 ) 2
ake
1—
0.314x10 -19
m
V 'o
1 - — | = 1.14 x 10 - 1 8 J = 7.12 eV/K + -Cl"
(b)
Atomic cohesive energy = ionic cohesive energy + energy needed to remove an
electron from Cl~ - energy gained by adding the electron to
K + = 7.12 eV + 3.61 eV - 4.34 eV = 6.39 eV/KCl.
83
84
CHAPTER 12
9
THE SOLID STATE
(a)
J - y'dt = -Ne-''f = -N[e~ -e°]
(b)
7 = _L J p . g-'/^f = T J Li. C-V* ™ = r J ze -^ z
jiw^w^wavv**
dv = e~2dz
v = -e~z
z=u
dz = du
so J ze~zdz = {-ze~z )|~ + J e~zrfz = 0 - <T2|~ = 1. Therefore, t = r.
o
o
12-11
(c)
Similarly £2 = — J
(a)
Equation 12.12 was / = nevd. As vd = nE, ] = nejuE. Also comparing Equation 12.10,
vd =
\e~^Tdt. Integrating by parts twice, gives t2 = 2r 2 .
, and vi=/jE, one has H = — .
me
me
(b)
As / = oE and / = / electrons + / h o i e s = nefi„ E + pejupE, a = neju„ + pejup
(c)
The electron drift velocity is given by
(d)
vd =//„£ = (3 900 cm2/Vs)(100 V/cm) = 3.9xl0 5 cm/s.
An intrinsic semiconductor has n = p. Thus
<T = neju„+peMp=pe(jUn+Mp)=:(3.0 xlO 13 cm _3 )(l.6xl0~ 19 C)(5 800 cm 2 /Vs)
= 0.028 A/V cm = 0.028 (Q cm) -1 = 2.8(Q m) _1
p = — = 0.36£2m
12-13
(a)
We assume all expressions still hold with vnas replaced by vF.
T
ne2
cr = l = (l.60xl0-8) \ilmy1=6.25xlQ7 (dm)-1
P
n=
#oie- J I T X
266 a . „ m . wm = v m 33 i - J ^ 3/ l kmole^
1n2
(6.02xlO
atoms/kmole)(l0.5xl0 kg/m )|
m3
^atom y
« = 5.85xl0 28 e ' / m 3
(6.25xl0 7 )(Qm)- 1 (9.11xl0- 31 kg)
so T=
5- = 3.80 x 10
(5.85xlO28 e7m 3 Xl.6xlO - 1 9 C)
Equation 12.10).
s (no change of course from
I
MODERN PHYSICS
(b)
'2£ \^2
Now L = vFt and vT = j — '2 x 5.48 eV x 1.6 x 10' 19 J/eV ~|1/2
v„ =
9.11xl(T 31 kg
= 1.39xl0 6 m/s.
L = (1.39 x 106 m/s)(3.8 x 10"14 s) = 5.27 x 1(T8 m = 527 A = 52.7 nm
(c)
The approximate lattice spacing in silver may be calculated from the density and the
molar weight. The calculation is the same as the n calculation. Thus,
(# of Ag atoms)/m 3 = 5.85 x 10 28 . Assuming each silver atom fits in a cube of side, d,
d3 =(5.85xl0 28 )~ 1 m 3 /atom
d = 2.57xl0 - 1 0 m
L 5.27 xlO" 8
w e
So- =
™ =205.
d 2.57 xlfT 10
c
12-15
(a)
E,=1.14eVforSi
hf = 1.14 eV = (1.14 eV)(l.6 x 10~19 J/eV) = 1.82 x 1(T19 J
/ = 2.75x10" Hz
(b)
c = Af;A^
/
=
3Xl 8 m S
° i /
-LWxlO^m
2.75xl0 1 4 Hz
A = 1090 nm (in the infrared region)
12-17
(a)
Potential
x =0
*• x
x=a
y/l=AeKx
Kh=[2m(U-E)]V2
yn = Bcosfct+Csinfct
kh = (2mE)l/2
Wm=De~Kx
In region I and III the wave equation has the form —*-»— = K2i/s(x) with
dx
1/2
[2m(LZ-£)]
_
.
.
,
_
,
.
,
,
,
v
K=
. This equation has solutions of the form
y/j (x) = AeKx for x < 0 (region I)
y/m = De'Kx for x > 0 (region III)
85
86
CHAPTER 12
THE SOLID STATE
In region II where U(x) = 0 we have — ^ 1 _ _
=
-k2y/(x) with k =
— . This
equation has trigonometric solutions
{/n(;t) = B cos Jet+ C sin
with k =
(2mE)V2
fcc
0<x<a
. The wave function and its slope are continuous everywhere, and
in particular at the well edges x = 0 and x = a. Thus, we must require
A=B
continuity of y/(x) at x = 0]
KA = kC
continuity of — — at x = 0
dx
continuity of y/{x) at x = a]
dy/{x)
continuity of —
at x = a
B cos kx + C sin kx - De~Kx
-Bk sin kx+Ck cos kx — -DKe-Kx
There are four equations in the four coefficients A, B, C, D. Use the first equation to
eliminate A. Then from the second equation we obtain B = I — C. Divide the last two
equations to eliminate D.
-Bfc sin fct+Q: cos fct DKe -Kx
Bcosfct+Csinfct
De_Kx
Cross multiply, gather terms and write B in terms of C. Then we have
-(f)|C cos ka - KC sin ka.
- — |Cfc sinfca+ Oc cos folic
Divide out C and gather terms to obtain (iC2 -k2)sinka
2m(U-E)
= -Ikacosk. Now substitute
1/2
cosfoz.This equation simplifies to:
II sin te = -2[E(U-E)] 1 / 2 cosfaj, which is a transcendental equation for the bound
energy states. Rearranging,
tan foz = tan'
(b)
(2mE)V2
4E(U-E)
L72
'
The energy equation is a transcendental equation and can be solved for the roots, E„
by using Newton's root formula as an iterative method employing a computer. If you
know the form of f(x) then you can approximate the value of x for which f(x) = 0.
Choose an initial value of x. The energy equation can be written as
/(E) = tan2
(2mE)1/2
a-[4E(LJ-E)]LJ r2 =0.
MODERN PHYSICS
87
In this problem approximate by using the energy for an electron in a well. The first
guess energy is: E„
2m„a + 2S
where
197.3 eVnm/c
5 = -~
= 0.019 3 nm
K 2(0.511 xlO 6 eV/c 2 )(100eV)
and so
rCitr (197.3 eV nm/c)
E =
" '- ^y"u EY " " ? " '
= n2(19 5eV)
6
2
2
" 2(0.511 xlO eV/c )(0.10 nm+0.039 nm)
E!=19.5eV
E2 = (2)2 (19.5 eV) = 78.0 eV
£ 3 = (3)2(19.5 eV) = 175.5 > U therefore unbound
These values seem reasonable since there are only two bound states. The next step in
Newton's method is to calculate f(x) and f\x) at the first guess value. Then use the
definition of slope and tangent:
=
/(s)
or x2 = x1 -
fix)'
Use x2 as a new estimate to evaluate %3, etc. Monitor x and f{x) for convergence and
divergence. Use the first term of two of the Taylor series for the first guess of /'(*).
Thus our first guess would be xx = E = 19.5 eV and
/(E) = tan2 to/ ( £ )
-UJl
4E(U-E)
U2
E J
cos 3 [( f l /n)(2m e E)V 2 ] + lLZ 2 r £
^
where Ji = 100 eV and E = 19.5 eV. Calculate x2 and keep repeating, watching for
convergence.
(c)
Potential
E< U
U
IV
III
x =0
a+b
2a + b
V
-> x
CHAPTER 12
THE SOLE) STATE
y/^AeKx
Kh = [2m(U-E)]y2
y/u = Bcoskx+Csm kx
kh = (2m£)1/2
^m=D^x
+ E'e-Kx
i//w = F cos kx+G sin kx
y/w=He~Kx
At x = 0, ^ = ipu. Therefore A = B, —^- = —^S- yields KA = kC. Similarly at x = a:
dx
dx
Wu = ¥ni / B cos ka+C sinto= De*0 + E'c - & and ^f&- = ^Zffi. ,
-Bit cosfa+Cfccos ka = KDeKa - KE'e-*". Substitute C = — and B = A to obtain
A cos *» + f — ] sinto= De*" + E'e-*1'
-Ak sin AH+(^ - 1 cos ka = KDe*" - KE'e - ^
Solve for A in each equation and equate quantities to obtain
De«° +
*£,
coste + (K/A;)sinfcfl
= KDe--
^
-/csinfan-Kcosfaj
Clear denominators and gather terms. After some algebra one obtains
D _ -K(cos ka+(K/a) sinfa)- (-k sin ka+K cos ka)e~Ka
E 7 " [-Jt sin *H + JC cos te-lC(co8fci + (X/ifc)8in *»)>*'
This can be simplified to obtain
D 2e-2Kfl[cositH + (l/2)[(K/it)-it/JiC]sin)tfl]
E'~
[(k/K)+K/k]smka
Impose the continuity conditions at x = a + b and let a = k(a + b) and
/3=K(a + b)
Vm = Vw
D^
+
EV^Fcosa + Gsina^ fcOS a a + G s i n g = l , a n d ^ B L = ^ ^
Dep + E'e~p
dx
dx
r,r-> /? r^rn/ -/?
r-i
^i •
-Ffc cos a+G/c sin a „
KDep + KE'e p = -Fkcosa+Gksma=^>
^
-R— = 1.
KDef+KE'e-P
Set quantities equal to 1 equal to each other and clear fractions to obtain
(F cos a+G sin a)(KDep + KE V s ) = {-Fk cos a+Gksin a)(De^ + E'e_/7).
MODERN PHYSICS
89
Divide by E' and gather terms to obtain
D
FK — cosa+ sin or
KE'J
UKAE'
= GK
S-Fk
cosfcor+ ( | ) s i n a
(Mf) C08a "(F) 8ina ? +GK [ B,na+ (llF) C0Ba }
Divide through by G and | — I to obtain
F _ (D/E')efi[cosa-(K/k)sma]
G (D/E')e^[sina+(K/k)cosa]
atx = 2a, i/xv = y/v,Fcosk(2a
+ e-^[cosa+(K/k)sina]
+ e ^[sinflf-(K//c)cosar]
+ b)+Gsink(2a + b) = He
and
and
dx
dx
dividing by (-K) we obtain — [Fk sin k(2a+ b)-G cos k(2a + b)] = He'**. Both equations
are equal to the same quantity so set equal to each other.
Fcos/c(2a + b)+Gsinfc(2a + b) = —[Ffcsinfc(2a + b)-GcosA:(2a + b)].
K
Now gather terms and divide by G and I
to obtain
F _ cos k(2a + b)+(K/k) sin k(2a + b)
G ~ sin Jk(2a + b) - (K/k) cos k(2a + b)'
Equating the two expressions for —
G
cos k(2a + b) + (K/fc) sinft(2a+ b) _ (D/E V [ c o s « - (K/fc) sin a] + e"^[cos g+(K/k) sin a]
sin k(2a + b)- (K/k) cos fc(2«+b) ~ (D/E')ep[sm a+(K/k) cos a] + e ^[sinor-(K/fc)cosa]
Bringing all terms to one side gives a transcendental equation in E
/(£) =
(D/E')ep[cos a - (K/k) sin a] + c~*[cos a+(K/k) sin a]
(D/E')e^[sin a+(K/k)cos or] + e_/?[sin a - (K/fc)cos a]
cosfc(2g+b)+(K/fc) sin k(a + b)
=0
sinfc(2a+b)- (K/fc) cos k(2a + b)
with U, a, and b as parameters. This equation can be solved numerically with Newton
roots method used in the solution to 12-17(b). The form of the program will depend
strongly on the computer language used, including its subroutine (function, module)
structure. Assume you can write a module to calculate /(E) where a = b -1 and
U = 100. Output tabular values of E and /(E) and/or graph E and /(E). The Newton
method requires both function and its derivative to be used. This is algebraically
complicated so that it proves more practical to use a more interactive program. Use
the computer to calculate /(E) for any E you enter. Use trial and error to converge to
CHAPTER 12
THE SOLID STATE
the values of £ for which/(£) changes sign. Those are the values of E, which satisfy
the equation and are the bound states of the double square well.
The search procedure is: Guess one value of £ and calculate /(£). Guess a second
value of E, not very different and calculate /(£). If the sign of /(E) changes,
interpolate a new E and calculate its /(E). If the sign of /(£) did not change,
extrapolate in a direction toward the smaller |/(E)|. Continue until AE, which causes
/(E) to change spin, is small enough for your needs. That is, less than 1 eV for this
problem, since you are looking for other splittings of the single-well energies at 19 eV
and 70 eV.
19
(a)
dm = _d_ f 2Ln | _ ( 2L Y dn_ _ tC
dX dX\ A ) [xkdX
AJ
Replacing dm and dX with Am and AX yields
. . X2Am{ Xdn
AX =
2L KdX
n
or \AX\ = — n
. Since AX is negative for Am = +1.
2L\
dX )
(b)
(c)
21
(a)
(837 xl(T 9 m) 2
-[3.58 - (837 nm)(3.8 x 10"* nm" 1 )] = 3.6 x 10 -10 m = 0.38 nm
\AX\ =
(0.6xl(T 3 m)
(633 xlO - 9 m) 2
= 6.7 x 10 -13 m = 0.000 67 nm = 6.7 x 10"4 nm
(0.6x10° m)(l)
The controlling factor is cavity length, L.
|AA|
See the figure below.
ft
0.540 T
23
(b)
For a surface current around the outside of the cylinder
as shown,
B£ (0.540 T)(2.50 x 10 -2 m)
B=
orM =
10.7 kA
Mo
(4^xl0" 7 ) T-m/A
(a)
AV = IR
If R = 0 , then AV = 0, even when 7 * 0 .
_w
MODERN PHYSICS
(b)
The graph shows a direct proportionality.
1507
100-
(mA)
5Q
0
1
(155-57.8) mA_ =
(3.61-1.356) mV
Slope = — =
R AV
2
3
AVcd (mV)
4 3 1 i r l
R= 0.023 2 Q
12-25
(c)
Expulsion of magnetic flux and therefore fewer current-carrying paths could explain
the decrease in current.
(a)
The currents to be plotted are
7D=(l0-6A)(eAV/0025V-l),/ w
2.42 V-AV
745 Q.
The two graphs intersect at AV = 0.200 V. The currents are then
ID = (10-* A)(eom
v
/ ° 0 2 5 v -1) = 2.98 mA
Diode and Wire Currents
-•-Diode
-•-Wire
S
cS3 J-U
mU
0^ » •
t
*
f
0.1
• - t - * i
0.2
1
0.3
AV (volts)
lw -
2.42 V-0.200 V
= 2.98 mA. They agree to three digits..-. ID=IW
745 £2
(b)
AV
0.200 V
^ =
ID 2.98 xlO" 3 A
67.1 n
(c)
d(AV)
dln
10"6 A ,0.200 V/0.025 V
0.025 V'
dip
d(AV)
8.39 Q
- 2.98 mA
91
f
13
Nuclear Structure
13-1
13-3
R = R0A1/3 where R0 = 1.2 fm;
(a)
A = 4 so RHe = (1.2)(4)1/3 fm = 1.9 fm
(b)
A = 238 so JRu = (1.2)(238)1/3 fm = 7.44 fm
(c)
Rv _ 7M fm
:3.92
R He
1.9 fm
PNVC
MNUCAW
/'ATOMIC
M ATOMIC / V A T O M I C
Pmc
= (^-)
'ATOMIC
^ATOMIC
and approximately; M^c
where r0 = 0.529 A = 5.29 x 10 -11 m and R = 1.2 x 10 -15 m (Equation 13.1
\RJ
where A = 1). So that PNVC
PATOMIC
13-5
(a)
= M ATOMJC . Therefore
'5.29x10"" m^ 3
= 8.57x10".
1.2 xlO - 1 5 m
The initial kinetic energy of the alpha particle must equal the electrostatic potential
energy of the two particle system at the distance of closest approach; Ka = U =—-—
and
(b)
rmin
_fa?Q
(9xl0 9 Nm 2 /C 2 )2(79)(l.6xnr 1 9 C)
~~K^~
[0.5MeV(l.6xl0 - 1 3 J/MeV)]
Note that K„
2kc,Q
v = mr „
mi
13-7
:4.55xl0 - 1 3 m.
1
2 fa?Q
—mv =—-—, so
1/2
2(9xlO 9 Nm 2 /C 2 )2(79)(l.6xl0 - 1 9 C) 2
4(1.67xlO"27 kg)(3xl0 - 1 3 m)
1/2
= 6.03xlO6 m/s
E = -ju • B so the energies are Ej = +/uB and E2 = -//B. ju = 2.792 8//„ and M„ = 5.05 x 10~27 J/T
AE = 2//B = 2x2.792 8 x 5.05 xlO - 2 7 J/Tx 12.5 T = 3.53xlO -25 1 = 2.2x10^ eV
93
94
CHAPTER 13
NUCLEAR STRUCTURE
13-9
We need to use the procedure to calculate a "weighted average." Let the fractional
/ 63 m( 63 Cu)+/ 65 m( 65 Cu)
abundances be represented by / 63 + / 65 = 1; then
—•———
= m Cu . We find
(/63 + /65)
m( 6 5 Cu)-m C u
6 4 9 5 u - 6 3 55u
/<» = / «
i
/M
x> / * =
-0.30 or 30% and / « = 1 - / « = 0.70 or 70%.
J63
J65
J63
m( 6 5 Cu)-m( 6 3 Cu) 63 64.95 u - 62.95 u
13-11
- ^ = i[l(1.007 276 u) + 2(1.008 665 u) - 3.016 05 u](931.5 MeV/u) = 2.657 MeV/nucleon
A 3
13-13
(a)
The neutron to proton ratio,
(b)
Using Eb = CXA - C 2 ^ 3 - C3 (Z(Z - 1)M"1/3 - C4 ( N ~ Z )
is greatest for
13
|Cs and is equal to 1.53.
the only variation will be in
the coefficients of C3 and C4 since the isotopes have the same A number. For
Eb =(15.7)(139)-(17.8)(139)^3 -0.71(59X139)^ -
23 6(21)
"
13
|Pr
=1160.8 MeV
139
- ^ = - ^ - = 8.351 MeV
A 139
For ^ La
Eb = (15.7)(139) - (17.8X139)^-0.71(55)(54)(139)1/3 - 2 3 , 6 ( 2 5 )
139
i k = - ^ - = 8.353 MeV
A 139
=1161.1 MeV
F o r ^55C s
£fc = (15.7)(139) -(17.8X139)^ - 0.71(55)(54)(139)V3 -
23,6(29)
139
=1154.9 MeV
• ^ = - ^ - = 8.308 MeV
A 139
139 La
(c)
13-15
has the largest binding energy per nucleon of 8.353 MeV
The mass of the neutron is greater than the mass of a proton therefore expect the
nucleus with the largest N and smallest Z to weigh the most: 13g Cs with a mass of
138.913 u.
Use Equation 13.4, Eb = [ZM(H) + Nmn - M( £x)]
(a)
For JgNe;
Eb =[10(1.007825 u) +10(1.008 665)-(19.992 436 u)](931.494 MeV/u) = 160.650
^ - = 8.03 MeV/nucleon
MODERN PHYSICS
(b)
95
For gCa
Eb =[20(1.007825 u) + 20(1.008 665) - (39.962 591 u)](931.494 Me V/u) = 342.053
•^• = 8.55 MeV/nucleon
(c)
For^Nb;
Eb = [41(1.007 825 u) + 52(1.008 665) - (92.906 377 u)](931.494 Me V/u) = 805.768
J
(d)
i>
_
8.66 MeV/nucleon
For : ^ A u
Eb = [79(1.007 825 u) +118(1.008 665) - (196.966 5431 u)](931.494 Me V/u) = 1559.416
-^- = 7.92 MeV/nucleon
17
A£ = E f c / -£ w
For A = 200; -^- = 7.8 MeV so
A
Ebi = (A,)(7.8 MeV) = (200)(7.8) = 1560 MeV
For A = 100; ^ - = 8.6 MeV so
A
Ebf = (2)(100)(8.6 MeV) = (200)(8.6) = 1720 MeV
AE = Ebf - £(,,- = 1720 MeV -1560 MeV = 160 MeV
19
(a)
kq
The potential at the surface of a sphere of charge a and radius r is V = —. If a thin
shell of charge d<7 (thickness dr) is added to the sphere, the increase in electrostatic
potential energy will be dU = Vdq = — \dq. To build up a sphere with final radius R,
the total energy will be 17 = J — \dq; where q-—n^p
Q\ T J
D
that
3k(Ze)2
5K
=—nrz
3
Ze
4;rK 3 /3
Flr
so
96
CHAPTER 13
(b)
NUCLEAR STRUCTURE
When N = Z = —,R = R0A^
and R0 = 1.2 x 10~15 m
_3k(Ze)2 _(3/5)(8.988xl0 9 Nm 2 /C 2 )(A/2) 2 (l.602xl0- 1 9 C) 2
U =
=
~5R~
(1.2 xlO- 15 m ) ^ 3
= 2.88xl0~ 14 (,4 5/3 )j
13-21
13-23
(c)
For A = 30, U = 8.3 x 1 0 ' " J = 52.1 MeV.
(a)
Write Equation 13.10 as — = e~xt so that A = - l n f - ^ - 1 . In this case -^- = 5 when
Rg
t \ RJ
R
t = 2 h, so A =—ln5 = 0.805 h _ 1 .
2h
(b)
In2=_jn2_
Ty2= — =
_, =0.861 h
A ~ 0.805 h _1
(a)
From R = V - * ' > *• = W ^ r l '
X
= ~\ln{~)
= 5 5 8 x 10 2 h _ 1 = 1JSS x 10 5 s _ 1 a n d
"
~
~
T1/2=^=12.4h.
13-25
(b)
R0 = 10 mCi = 10 x 10~3 x 3.7 x 1010 decays/s = 3.7 x 108 decays/s and R = AN so
„
RQ 3.7xlO 8 decays S"1 „„„ ,„ 1 3
N„ = -f- =
T ^ T — = 2.39 x 1013 atoms
u
-5 _1
A
1.55xlO s
(c)
R = R0e~*' =(10 mCi)e-^xW^m
=1.87 mCi
Combining& Equations
13.8 and 13.11 we have N = '—'—!•=—'—'—J— and since
n
A
0.693/T1/2
l m C i = 3.7xl0 7 decays/s.
(5mCi)(3.7xl0 7 dps/mCi)
N=
-—i
*-i=7
4 y = 2.43xlO 17 atoms
7
0.693/[(28.8yr)(3.16xl0 s/yr)]
Therefore, the mass of strontium in the sample is
N ..
m = —M =
13-27
2.43xlO17 atoms
23
.„„
. , . n, „ „ <
( 9 0 g/mole) = 36.3XKT6 g.
Let R0 equal the total activity withdrawn from the stock solution.
R0 =(2.5 mCi/ml)(10 ml) = 25 mCi.
'
MODERN PHYSICS
Let R'0 equal the initial specific activity of the working solution.
After 48 hours the specific activity of the working solution will be
R' = Jtyf*'=(0.1 mCi/ml)e- (a693/15h)(48h) = 0.011 mCi/ml
and the activity in the sample will be, R = (0.011 mCi/ml)(5 ml) = 0.055 mCi.
13-29
The number of nuclei that decay during the interval will be
N1-N2=N0(e-M'-e~Mi).
First we find X;
A=
Jn2 = 0693_
T1/2 64.8 h
R0
x=197xl0-6
(40//Ci)(3.7xlO 4 d p s / / 0 )
2.97 X H T S - 1
-i
and
= 4.98 xlO 11 nuclei
Using these values we find
N, - N 2 =(4.98xlO n )[e-( 0 0 1 0 7 h " ) ( 1 0 h )
-e-i°*™W™'.
Hence, the number of nuclei decaying during the interval is
Nj -N2 = 9.46xlO 9 nuclei.
13-31
(a)
c/m
300
200
0 1 2 3 4 5 6 7 8 9
Time (hr)
10 11 12
(b)
^ ^ - s l oFp e ^ - l n 2 Q Q " l n 4 8 0 =0.25 hr' 1 =4.17xl0" 3 min"1 and Tyz1/2 = - ^ = 2.77 hr.
(12-4) hr
X
(c)
By extrapolation of graph to t = 0, we find (cpm)0 = 4 x 103 cpm
(d)
R
R„ (cpm)n/EFF
N = ^ - ; N 0 = ^ =^ - ^
4xl04dis/min
4.17xlO -3 min - 1
59xl()6atoms
97
98
CHAPTER 13
13-33
(a)
NUCLEAR STRUCTURE
Referring to Example 13.11 or using the note in Problem 35 R = R0e
Xi
,
RQ = NQX = 13xlO~12NQ(12C)X
f
Rn
where X =
1.3 x 10"12 x 25 g x 6.02 x 1023 atoms/mole"
X
12 g/mole
:
=- = 3.84 x 10~12 decay/s. So RQ = 376 decay/min, and
5 730x3.15xl0 7
R = (3.76xl0 2 )exp[(-3.84xl0" 12 s _ 1 )x(2.3xl0 4 y)x(3.15xl0 7 s/y)]
R = 18.3 counts/min
(b)
13-35
The observed count rate is slightly less than the average background and would be
difficult to measure accurately within reasonable counting times.
First find the activity per gram at time t = 0, R0 = N0 ( u C), where
N 0 ( 14 C) = 1.3xl(T 12 N 0 ( 12 C); and N 0 ( 1 2 C) = f — V . . Therefore %L = (^-1(1.3xl(T12)
\MJ
m \ M J
and
the activity after decay at time t will be — = f - ^ - V A ' = f - ^ 0 ( 1 . 3 x l O - 1 2 ^ ' where
X = — = 2.3 x 10 -10 min"1 when f = 2 000 years.
^1/2
R
m
f3.2xl0 - 1 0 min'M ( 1 . 3 X 1 0 - 1 2 ) ( 6 . 0 3 X 1 0 2 3
\
12 g/mole
m o l e -l) x e -(3-2xlO-
10
nun-')(2000 y ) (5.26 X ^ mir^y)
— = 11.8 decays min
min"_11g" -1
m
13-37
(a)
Let Nt = number of parent nuclei, and N2 = number of daughter nuclei. The
daughter nuclei increase at the rate at which the parent nuclei decrease, or
dN2 = XN01e-x'tdt
N2 = X N 01 J e~Xldt = -N01e-Xt + Const.
If we require N 2 = N 02 when t = 0 then Const = N 02 + N 0 1 . Therefore
N 2 = N 02 + N 01 -N 0 1 e~ x t . And when N02 = 0; N 2 = N 0 ] ( l - e ~ X t ) .
(b)
Obtain the number of parent nuclei from N1 = N01e Xt and the daughter nuclei from
, _ l n 2 _ 0.693
N 2 = N 01 (1 - e ~ M ) with N01=W6,X = — = ^ - = 0.069 3 h" 1 . Thus the quantities
" Ty
Ty22 ~ 10
10 hh
Ni=1()6e-(0.0693h
-)'
a n d N 2 = 1 { )
6 ',
-(0.0693 h _1 )f'
are plotted below.
MODERN PHYSICS
10
0.0
20
99
30
f(hours)
13-39
A number of atoms, dN-X Ndt, have life times of t. Therefore, the average or mean life time
At
will be I ( d N ) - i - or jdN^- so T = ^-]xNtdt
= ^~]xN
0e- tdt = \ .
£dN
NQ
N0J0
N0 J0
X
13-41
Q = ( M 2 3 8 u - M 2 M T h - M 4 H e ) ( 9 3 1 . 5 MeV/u)
= (238.048 608 u - 234.043 583 u - 4.002 603 u)(931.5 MeV/u) = 2.26 MeV
13-43 (a)
We will assume the parent nucleus (mass Mp) is initially at rest, a n d we will denote
the masses of the daughter nucleus and alpha particle by Md and M a , respectively.
The equations of conservation of momentum and energy for the alpha decay process
are
Mdvd=Mava
Mpc2 = Mdc2+Mac2
(1)
+[jJMdv2d+{~JMav20
(2)
The disintegration energy Q is given by
Q = (Mp -Md -Ma)c2
=[\)Mdv2
+(|]MoDl
Eliminating vd from Equations (1) and (3) gives
QH-IM,
Q
Mc
rM2^
\Mdj
+ \~\Mavl
vl+[^\Mavl
Q = g > X1 + M^ L
'^d J
Q
1 + Ma/M
4.87 MeV
= 4.79 MeV
1 + 4/226
(b)
K,
(c)
Kd = (4.87 - 4.97) MeV = 0.08 MeV
Md
(3)
100
CHAPTER 13
(d)
NUCLEAR STRUCTURE
For the beta decay of 210 Bi we have Q = Kg. 1 + —£- . Solving for Ke. and
substituting Me_ = 5.486 x 10"4 u and M Y = 209.982 u (Po), we find
1 + 5.486 x 10"4 u/209.982 u
1 + 2.61 x 10""6 '
Setting 2.61 x 10"* =e, we get Kg_ =Q(l + f)" 1 = Q ( l - e ) = Q(l-2.61xlO - 6 ) f o r f « l .
This means the daughter Po carries off only about three millionths of the kinetic
energy available in the decay. This treatment is only approximately correct since
actual beta decay involves another particle (antineutrino) and relativistic effects.
13-45
Q = (m initial -m final )(931.5 MeV/u)
(a)
Q = fn(^Ca)-m(e + )-m(^K) = (39.962 59 u - 0.000 548 6 u - 39.964 00 u)(931.5 MeV/u)
= -1.82MeV
Q < 0 so the reaction cannot occur.
(b)
Using the handbook of Chemistry and Physics
Q = m ( ^ R u ) - m ( 4 H e ) - m ( ^ M o ) = (97.9055 u-4.0026 u-93.9047 u)(931.5 MeV/u)
= -1.68MeV
Q < 0 so the reaction cannot occur.
(c)
Using the handbook of Chemistry and Physics
Q = m( JJ* N d ) - m ( | He) -m(^°Ce) = (143.909 9 u-4.002 6 u -139.905 4 u)
x (931.5 MeV/u) = 1.86MeV
Q > 0 so the reaction can occur.
13-47
We assume an electron in the nucleus with an uncertainty in its position equal to the nuclear
diameter. Choose a typical diameter of 10 fm and from the uncertainty principle we have
Ap = — = 6.6xl0 - 3 4 Js/l0~ 14 m = 6.6xl0 _20 N s .
Ax
Using the relativistic energy-momentum expression
E2 = (pc) 2 + (m 0 c 2 ) 2
we make the approximation that pc ~(Ap)c»m0c2
so that
£ = pc = (A p)c = (6.6 xl0~ 20 Ns)(3xl0 8 m/s) = 19.8xKT 12 J = 124MeV.
However, the most energetic electrons emitted by radioactive nuclei have been found to have
energies of less than 10% of this value, therefore electrons are not present in the nucleus.
MODERN PHYSICS
13-49
101
The disintegration energy, Q, is c 2 times the mass difference between the parent nucleus and
the decay products. In electron emission an electron leaves the system. That is
z X ->z+i Y + e~ + v where v has negligible mass and the neutral daughter nucleus has
nuclear charge of Z +1 and Z electrons. Therefore we need to add the mass of an electron to
get the mass of the daughter. The disintegration energy can now be calculated as
Q=
{MzxX-M[zi+1Y-me]-me+0}c2={M2X-M$+1Y}c2.
Similar reasoning can be applied to positron emission z X -*z-i Y + e+ + v and so
Q=
{MiX-M[l1Y-me}-me+0}c2=[M^X-Mt1Y-2me]c2.
For electron capture we have ^ X + e ' ^ Y + u , which gives
Q = {MzxX + me-M[tiY+tne}
13-51
0}c2=[MzxX-Ml1Y]c2.
+
In the decay jH->2 He+ e + u the energy released is: E = (Am)c 2 =[M 1 H -M 3 H e ]c 2 since the
mass of the antineutrino is negligible and the mass of the electron is accounted for in the
atomic masses of JH and \ He. Thus,
E = (3.016 049 u - 3.016 029 u](931.5 MeV/u) = 0.018 6 MeV = 18.6 keV.
Nn, = 1.82xl0 10 ( 87 Rb atoms/g)
13-53
N Sr =1.07xl0 9 ( 87 Sr atoms/g)
r 1 / 2 ( 8 7 Rb-£-^ 8 7 Sr) = 4.8xl0 10 y
(a)
If we assume that all the 87Sr came from
1 82xl0
10
87
Rb, then N&, = N0e~M
=(l.82xl0 1 0 +1.07xl09)e-(In2/4-8><10,0)'
-ln(0.94447) = f ^ 1.0, \
U.8xl0 ;
f = 3.96xl0 9 y
13-55
(b)
It could be no older. The rock could be younger if some
(a)
Starting with N = 0 radioactive atoms at t = 0, the rate of increase is (productiondecay)
™ = R-AN
dt
dN = {R-AN)dt
Sr were initially present.
102
CHAPTER 13
NUCLEAR STRUCTURE
Variables are separable
R-XN
R
R-XN
R
H
-Xt
-XI
i-ity-r*
N:
(b)
^
N
1
13-57
<!>--">
= R-XNmax
=*
max
i
We have all this information: Nx (0) = 2.50NV (0)
N I (3d) = 4.20Ny(3d)
NI(0)<T/l*3d =4.20Nuy(0)<f/l'3d =4.20-^^-e" / l ! ' 3 d
2.50
e3<u, _ 2 3 ^ y
4.2
[2.51
3dA x =ln
+ 3dAy
.4.2.
,,0.693 . f2.5 ^ O J 0.693
: 0.781
3d
= ln — +3d
T1/2x2
U.2J
1.60 d
7
i/2^= -66d
13-59
N = N0e'Xt
dN
= K = |-AN0e"/lf \ = R0e-xt
dt
R
A f = hB>V—*
U J T1/2
f _T
'1/2
HR„/R)
In 2
If R = 0.13 Bq,
t = 5 730 y r ^ ^ f f i = 5 406 yr.
4
'
0.693
*
IfR = 0.11Bq, t = 5 7 3 0 y r ^ ^ > = 6 7 8 7 y r .
^
'
0.693
*
The range is most clearly written as between 5 400 yr and 6 800 yr, without understatement.
MODERN PHYSICS
13-61
(a)
103
Let N be the number of m U nuclei and N ' be 206 Pb nuclei. Then N = N 0 e _/tf and
N 0 = N + N' so N = (N + N')e~M or eXi = 1 + — . Taking logarithms, X t = lnf 1 + — )
N
\
NJ
where X =
. Thus, t
lnf 1 + — ) . If ~ = 1.164 for the ^ U -» ^ P b chain
vln2y
'1/2
V Ny
N
9
with T1/2 = 4.47 x 10 yr, the age is:
4.47xlO 9 yr"
In 1 + ln2
1.164
J
N'
It
(b)
From above, e
N
iV
iV
= 4.00xl0 9 yr.
N
IN
= 1 + — . Solving for —- gives —- -
-xt
With t = 4.00xlO 9 yr
_A(
and T1/2 = 7.04xlO8 yr for the 235 U-» 207 Pb chain,
9
^
'ln2^ (In2)(4.00xl0 yr)
i
—'—!- = 3.938 and — = 0.019 9.
At =
85
7.04xl0 yr
N'
\Jyij
With t = 4.00x10" yr and Ty2 =1.41xl0 l u yr for the ^ T h - ^ P b chain,
(In2)(4.00xl0 9 yr)_
At =
TT:
1.41xl0 10 yr
=
0.196 6 a n d — = 4.60.
N'
I"
*
14
Nuclear Physics Applications
14-1
18
18
0 = 17.999160
F = 18.000 938
*H = 1.007825
mn =1.0086649
14-3
all in u.
(a)
Q = [ M 0 + M H + M F - m n ]c 2 = [-0.002 617 9 u] [931.494 3 MeV/u] = -2.438 6 MeV
compared to -2.453 ± 0.000 2 MeV.
(b)
Kth=-Q
1.007825
1 +MR = (2.438 6 MeV) 1 +
M
17.999160
xJ
: 2.5751 MeV
Q = (M„ +M ( , B e ) - M ( I 2 c ) -M n )(931.5 MeV/u)
= (4.002 603 u+9.012182 u -12.000 000 u -1.008 665 u)(931.5 MeV/u)
Q = 5.70 MeV
14-5
Q = (ma+mx-mY-mb)[931.5
Q=
m
( ' H ) + m ( 7 L i ) - ' " ' * He)-™*
MeV/u]
u[931.5 MeV/u]
Q = [1.007 825 u + 7.016 004 u - 4.002 603 u - 4.002 603 u] [931.5 MeV/u]
Q = 17.35 MeV
14-7
(a)
Q = [m( u N) + m( 4 He)-m( 1 7 0)-m( 1 H)](931.5MeV/u)
Using Table 13.6 for the masses.
Q = (14.003 074 u + 4.002 603 u -16.999132 u -1.007 825 u)(931.5 MeV/u)
Q =-1.19 MeV
K .._4<*M"N)]
M
m[ N )
(b)
r
V
.002603
4
1.003074
I
-'
= 1.53 MeV
Q = [m( 7 Li)+m( 1 H)-2m( 1 He)](931.5 MeV/u)
Q = [(7.016 004 u +1.007 825 u) - (2)(4.002 603 u)](931.5 MeV/u)
Q = 17.35 MeV
105
106
CHAPTER 14
14-9
(a)
NUCLEAR PHYSICS APPLICATIONS
CM SYSTEM
V
Ma
Mx
X
2
2
2Ma
2
2MX
Mx + Ma
MaMx
2
LAB SYSTEM
v +V
My
At
P]ah=Ma(v + V)(Eq. 1)
M^ + M,,
=P
K,lab
M,
VL _P 2 [K + Mfl)/Mj2
2M„
Comparing to K^,
(b)
for substituting » = -£— and V = ——• in Eq. 1.
2M„
K bb =K CM
M z + Ma
M,
M.
orX(h=-Q 1 +
M,
V '"* /
First calculate the Q-value
Q = [m( 14 N) + m( 4 He)-m( 1 7 0)-m( 1 H)](931.5 MeV/u)
Q = [14.003 074 u + 4.002 603 u -16.999132 u -1.007 825 u](931.5 MeV/u)
Q = -1.19MeV
Then
m( 4 He)
1+— 14 m( N)
K t t =-(-1.19MeV) 1 +
14-11
R = R0e~nc7X, x = 2m, J R = 0.8R 0 ,n =
/?
m atom
_
4.002 603
14.003074
:1.53MeV
70 kg/m :
i28 _ - 3
_27 , =4.19x10^ vcT, 0.8R0 =R 0 e
1.67x10"" kg
0.223
Q.8 = e~ncx, nax = -ln0.8, <r=— ln(0.8) =
4.19xlO28 m ~ 3 x 2 m
2.66xl0 _ ; , u m z = 0.026 6 b
-
MODERN PHYSICS
14-13
107
Equation 14.4 gives R = (R0nx)a. Using values of E and a, we have
(a)
2*!! = £12. = 0.037 3,
*i
(b)
A_
0i
=
0.066 3, and
^o.i
14-15
(C)
-?!Li_.i
(d)
Therefore we can use cadmium as an energy selector in the range 0.1 eV to 10 eV to
detect order of magnitude changes in energy.
(a)
— = e~nax', x = thickness in m, cr= cross section in m 2 and
N0
n = # gold nuclei/m 3
n = (6.02xl0 23 atoms/mole)(l mole/197 g)(l9.3 g/cm 3 )
n = 5.9xl0 22 atoms/cm 3 = 5.9 xlO 28 atoms/m 3
Taking x = 5.1 x 10~5 m, we get
— = exp(-5.9xl0 28 atoms/m 3 x500xlO - 2 8 m 2 x5.1xl0~ 5 m) = 0.86
(b)
N = 0.86N0
N0=6.3xlO
(c)
14-17
n
N 0 = 7 T 5 ^ T-1 9
1.6X10 * C
protons/s
and
N = 6.1xl0 n protons/s
The number of protons abs. or scat, per sec 0.14N0 = 8.7xlO10 protons/s
Since N = N0e~n<TX, — = -Nnccr, where N = neutron density, nc = cadmium nuclei density,
dx
and cris the absorption cross-section. Thus,
= -Nncavth where vth is the neutron
V at Ja
—-—-—
thermal velocity given by vth = ———
I m„ )
. The
The neutron
neutron decav
decay rate.
rate,
, comes from
\dt JD
differentiating N = N 0 e - / l ( / ^ l =-NA where /l = - ^ - = - ^ ^ = 1.09xl0- 3 s" 1 .Finally
v dt JD
Ty2
636 s
(dN/dt)a _ -Nncavth _ ncovih
{dN/dt)
-NA
X
108
CHAPTER 14
NUCLEAR PHYSICS APPLICATIONS
As nc = (8.65 g/cm 3 )(6.02 x 1023 nuclei/112 g)
cr=(2450b)(l0' 2 4 cm 2 /b)
(1.5)(l.38xl0 -23 J/K)(300 K ) l V 2
Vtu =
1.67xl0 -z/ kg
A = 1.09xl0 -3 s - 1
(dN/dt)n
12
- — ^ - = 2.25xl0 12
(dN/dt)D
14-19
ET = E(thermal) = -kBT = 0.038 9 eV. ET = ( - j E where n = number of collisions, and E is the
initial kinetic energy. 0.0389 = (— J (lO6). Therefore n = 24.6 or 25 collisions.
14-21
AE = c 2 (mu -m^-m^
-mn)
AE = (931.5 MeV/u)[235.043 9 u -140.913 9 u - 91.897 3 u - 2(1.008 7 u)]
AE = (931.5 MeV/u)[0.215 3 u] = 200.6 MeV
14-23
14.25
(a)
w
Forasphere:V = - ; r r 3 a n d r = ( — )
^
3
U;zJ
,so — = ^
, =4.84y 1 / 3 .
V (4/3>rr 3
(b)
For a cube: V = Z3 and / = V 1 ^ s o A = ^ _
F Z3
(c)
For a parallelepiped: V = 2a 3 and a = (2V)1'3, so ~ = — — p ~ = 6.30V"1''3.
(d)
Therefore for a given volume, the sphere has the least leakage.
(e)
The parallelepiped has the greatest leakage.
(a)
eff = ?delivered = 0.3, Pout = * 0 ° ° M W = 3 333 MW
P0ut
0.3
(b)
Pheat = Pout - Pdelivered = 3 333 - 1 000 = 2 333 M W
(c)
The energy released per fission event is Q = 200 MeV. Therefore
= 6 y-V3
A
_ Pout
Q
=
2a2+8fl2
3.333 3 x 109 W/200 MeV
1.6 xlO - 1 3 J/MeV
Rate = 1.04 xlO 20 events/s
MODERN PHYSICS
(d)
109
235 xl(T 3 kg/mole "
(time)
6.0 xlO 23 atoms/mole
M = (Rate)
M = (l.04xl0 20 events/s)(3.92xl0 -25 kg/atom)(365 days)(24 h/day)x(3 600 s/h)
= 1.34xl0 3 kg
(e)
dM flYdE\
3.333 x l O y W
- — = — — =—
= 3.7 x 10_B kg/s. To compare with (d) we need the
dt Vc AdtJ
(3xl0 8 m/s)
mass for a year.
^ ( y e a r ) = (3.7 x 10 -8 kg/s)(365 days)(24 h/day) x (3 600 s/h) = 1.17 kg.
This is 8% of the total mass found in (d).
14-27
= rD+rT= (1.2 x 10~15 m)^ 1 / 3 + 31/3) = 2.70 x 10"15 m
(a)
r
(b)
(9xl0 9 N m 2 / C 2 ) ( l . 6xiu
x l 0 -"1 9 Ce )s 2
kez
U = — = -i
£
^- = 1.15xl0- 13 J = 720keV
2xl0-ls m
(c)
Conserving momentum: vf = —-—-—
mD +mT
(1)
(d)
1 vl=-{m
j J , +m
. )v$+U
, . U2
-m
D
D
T
(2)
Eliminating vv from (2) using (1), gives
(mD\
12/
2
1,
2
.
1
vlmn
(mD+mT)
1T
1
-{mD + mT)mDvl — - m 2 , ^ =(m D + m r ) U o r
1
m272_(mD+mT
—mDL,v0U 2
2
14-29
A
5,,
5
LZ = -L7 = -(720keV)
m^^l^MeV.
(e)
Possibly by tunneling.
(a)
Q = X a + Kn = 17.6 MeV = (1.2)m„ u 2 +—m„ u 2 . Momentum conservation yields
mnv„ = mava. Substituting va = ——vn into the energy equation gives Kn =
Ka
a
(b)
. ^ Q .
m„ + m„
Finauy,
'
K„ = <4.«PX17.6 MeV)
"
4.003 + 1.009
-—
MeV, Ka =3.45 MeV.
Yes, since the neutron is uncharged, it is not confined by the B field and only Ka can
be used to achieve critical ignition.
110
CHAPTER 14
14-31
(a)
NUCLEAR PHYSICS APPLICATIONS
The pellet contains
UxR^
v
(0.2 g/cm 3 ) =
^4^(0.5 xlO" 2 cm)
(0.2 g/cm 3 ) = 1.05xl0 _ 7 g
u
3
of 2j THT +, \H
"molecules." The number of molecules, N, is
T
'1.05x10-^
(6.02 x 1023 molecules/mole) = 1.26 x 1016.
5.0 g/mole
Since each molecule consists of 4 particles ( \ H , 3 H, 2e ), £ = (4N)—fcBT or
Zi
0.01(200 xlO 3 J)
Y—
—
1
J.
= 19x10 K
6NfcB 6(1.26 xl0 16 )(l.38xMT 23 J/K)
E
14-33
(b)
The energy released = (17.59 MeV)(l.26 x 1016 )(l.6 x 10 -13 J/MeV) = 355 kj.
(a)
Roughly — (15 x 106 K) or 52 x 106 K since 6 times the coulombic barrier must be
(b)
surmounted.
Q = Amc2 = (12.000 000 u +1.007 825 u -13.005 738 u)(931.5 MeV/u)
Q = 1.943 MeV
The other energies are calculated in a similar manner and the total energy released is
Zi
(1.943 +1.709 + 7.551 + 7.297 + 2.242 + 4.966) MeV = 25.75 MeV.
The net effect is 12C + 4p ->12,C + ^He.
(c)
14-35
Most of the energy is lost since v' s have such low cross-section (no charge, little mass,
etc.)
Total energy = number of 6 Li nuclei (22 MeV)
'6.02xl0 2 3 nuclei)
= (0.075)(2xl0 -13 g)
1(22 MeV)(l.60 x 1013 J/MeV) = 5.3 x 1023 J
About twice as great as total world's fuel supply.
14-37
(a)
N = number of 3 H,
(3xl0~ 3 gjfimxlO23
pairs/mole)
]Hpairsin3mg = 5.0 g/mole
= 3.61x20 zu pairs.
PowerOutput =(10)(0.3)(3.61xl020)(17.6 MeV/fusion)(l.60xl0 -13 J/MeV)/s
= 3.1xl0 9 W
Power Input =(10)(5xl0 14 j/s)(l0 - 8 s)/s = 5xl0 7 W
Net Power =(3.1xl0 9 - 5 x l 0 7 ) W = 3.0xl0 9 W = 3000MW
MODERN PHYSICS
(b)
14-39 (a)
14-41
111
1 day's fusion energy = (3 000 MW)(3 600 s/h)(24 h/day) = 2.6 x 1014M J. This is
26xl014 I
equivalent to
'•—-.
= 5.2 x 106 liters of oil or 5 million liters of oil!
6
50xl0 J/liter
„
far2Z,Z2
(9xl0 9 Nm 2 /C 2 )(l.6xl0- 1 9 C) 2 Z 1 Z 2
10"
14
„
m
(b)
D-D and D-T: Zx = Z 2 = 1 and £ = 2.3 x 10~1V J = 0.14 MeV
(a)
E = (931.5 MeV/u)Am = (931.5 MeV/u)[(2 x 2.014102) - 4.002 603] u. £ = 23.85 MeV for
every two 2 H ' s .
(3.17xl0 8 mi3)[(5 280 ft/mi)(12 in/ft)(0.025 4 m/in)] 3 [l0 6 g ( H 2 0 ) / m 3 ]
x[6.02xl0
2g(H)
[18 g(H 2 0)
protons/g(H)](0.0156 H/proton)(23.85 MeV/ H)(l.6xlO" 13 J/MeV)
23
2
2
= 2.63xl0 33 J
f2.63x!0 33 J Y
year
,.
„
=— = 119 billion years
7xl0 1 4 J / s J l 3 . 1 6 x l 0 7 s ;
'
14-43 (a)
(b)
1014 s/<cm
Is
:10M/lcm
2nJtBT = (2xl0 1 4 /cm 3 )(l.38xl0- 2 3 J/K)(8xl0 7 K)(l0 6 cm 3 /m 3 )
2nfcBr = 2.2xl0 5 j / m 3
14-45
(c)
- = 10(2nfcBT)
B=[20//0(2nitBT)]1/2
2//(
B = [20(4^xl0" 7 N/A 2 )(2.2xl0 5 j / m 3 ) ] ' =2.35T
(a)
For the first layer: 7a = I0e~(M'^), for the second layer: I2 = he
layer: ^- = I2e-^
n)d
14-47
" , and for the third
+
so that ^- = loe- ^ "^ f^. Using Table 14.2,
ln3
MM + Men + Mn
(b)
d +
{Mc d)
ln3
:1.4xl0~ 3 cm.
_1
(5.4+170 + 610)(cm )
If the copper and aluminum are removed, then I = j^-f 6 1 0 ^ 4 0 * 1 0 " 3 ) = 0 .426/ 0 . About
43% of the x-rays get through whereas 33% got through before.
In2 ln2
= — = 3.85 cm
M 0.18
This means that x-rays can probe the human body to a depth of at least 3.85 cm without
severe attenuation and probably farther with reasonable attenuation.
x=
112
CHAPTER 14
NUCLEAR PHYSICS APPLICATIONS
14-49
(a)
Assume he works 5 days per week, 50 weeks per year and takes 8 x-rays per day. # x5
rays = 2 000 x-rays per year and
= 0.002 5 rem per x-ray.
2000
(b)
5 rem/yr is 38 times the background radiation of 0.13 rem/yr.
14-51
The second worker received twice as much radiation energy but he received it in twice as
much tissue. Radiation dose is an intensive, not extensive quantity—measured in joules per
kilogram. If you double this energy and the exposed mass, the number of rads is the same in
the two cases.
14-53
One rad -> Deposits 10 "2 J/kg, therefore 25 rad -> 25x10~2 J/kg
If M = 75 kg, E = (75 kg)(25 x 10 -2 J/kg) = 18.8 J
14-55
One electron strikes the first dynode with 100 eV of energy: 10 electrons are freed from the
first dynode. These are accelerated to the second dynode. By conservation of energy the
number freed here, N is: (10)(AV) = (N)(10) or 10(200 -100) = N(10) so N = 100. By the
seventh dynode, N = 106 electrons. Up to the seventh dynode, we assume all energy is
conserved (no losses). Hence we have 10s electrons impinging on the seventh dynode from
the sixth. These are accelerated through (700 - 600) V. Hence E = (lO6 )(100) = 108 eV. In
addition some energy is needed to cause the 106 electrons at the seventh dynode to move to
the counter.
14-57
To conserve momentum, the two fragments must move in opposite directions with speeds vl
and v2 such that
wijDj =m2v2
or
v2 =
The kinetic energies after the break-up are then Kj = i m 1 u 2 and
1 m „2
_ 1. fm ^ v\
K2 =-£j-tn
2v2 =-2^2
\mu
The fraction of the total kinetic energy carried off by ml is
JC1
KJ+KJ
Kt
K1+(m1/m2)K1
and the fraction carried off by m2 is 1
14-59
'
ml+m2
m
mx+m2
m1+tn2
2,
(a)
AV = 4;rr2Ar = 4^(14.0 x 103 m) (0.05 m) = 1.23 x 10* m 3 ~ 108 m 3
(b)
The force on the next layer is determined by atmospheric pressure.
W = PAV = (1.013 x10 s N/m 2 )(l.23xl0 8 m 3 ) = 1.25xl0 13 J~10 1 3 J
MODERN PHYSICS
(c)
(d)
1.25 x 1013 J =—(yield), so yield = 1.25 x 1014 J ~ 1014 J
1 2Sx1fl* 4 T
'
= 2.97 x 104 ton TNT ~ 104 ton TNT or ~ 10 kiloton
4.2xlO J/tonTNT
9.
113
s
15
Particle Physics
15
15-1
The time for a particle traveling with the speed of light to travel a distance of 3 x 10
., d _ 3 x l 0 ' 1 5 m
«,
8s
At = —=
=
10
s.
v 3 x l 0 m/s
15-3
The minimum energy is released, and hence the minimum frequency photons are produced.
The proton and antiproton are at rest when they annihilate. That is, E = £ 0 and K = 0. To
conserve momentum, each photon must carry away one-half the energy. Thus,
2F
= £ ° = 9383
Enun = Vmta = ~f
M e V
'
TllUS
m is
'
(938.3 MeV)(l.6xlO- 19 J/MeV)
6.63 xlO - 3 4 Js
and
c
3 x l 0 8 m/s _
=
=
'•-max " ; —
vi
1-32 x 10
23
/min 2.26 xlO Hz
=
15-5
u
m
The rest energy of the Z° boson is £ 0 = 96 GeV. The maximum time a virtual Z° boson can
exist is found from A£Af = h.
A1
h
Af =
=
A£
1.055xlO-34 J s
;
,77
^ 0 ^ nn _ 27
^ = 6.87x10 Z7 s.
(96GeV)(l.6xl0~ 10 J/GeV)
The maximum distance it can travel in this time is
d = c(A0 = (3xl0 8 m/s)(6.87xl0" 27 s) = 2.06xl0" 18 m.
The distance d is an approximate value for the range of the weak interaction.
115
116
CHAPTER 15
PARTICLE PHYSICS
15-7
Use Table 15.2 to find properties that can be conserved in the given reactions
Reaction 1
;r"+p-»K"+2;+
(_) + (+)_>(_) + (+)
0->0 V
Reaction 2
n~ + p -» n~ + Z +
(-) + ( + ) ^ (-)+(+)
0->0 V
(a)
Charge:
(b)
Baryon number:
(0) + (+l)->(0) + (+l)
+l->+l V
(0) + (+l)->(0) + (+l)
+1 -> +1 /
(c)
Strangeness:
(0) + ( 0 ) ^ ( + l ) + (-l)
0->0 v'
(0) + (0)->(0) + (+l)
0->(-l)X
Thus, the second reaction is not allowed since it does not conserve strangeness.
15-9
15-11
,,.„
15-13
(a)
p -> n~ + tc°
(Baryon number is violated: 1 -> 0 + 0)
(b)
p + p - > p + p + ;r0
(This reaction can occur)
(c)
p + p -» p + 7t+
(Baryon number is violated: 1 +1 —> 1 + 0)
(d)
K+ -> JU+ + VM
(This reaction can occur)
(e)
n -> p + e~ + ve
(This reaction can occur)
(f)
jt+
(a)
ju~ -^e+y
Le: 0 - > l + 0 andL^: l - > 0 + 0
(b)
n - » p + e ~ + ve
Le:0->0 + l + l
(c)
A ° ^ p + ^°
Strangeness -1 -»0 + 0 and charge 0 -» +1+0
(d)
p->e++n°
Baryon number +1 -> 0 + 0 and lepton number 0 -»1+0
(e)
H ° ^ n + ^°
Strangeness -2 -> 0 + 0
,,
(a)
, c
a ici£ v
(m3+tni+m5+m6)2c2
-(m1+m2)2c2
.
. ^,
2
2
In Equation 15.16, Kth = ±-^
sJ.
b__i
U
where mx is the mass
2m 2
of the incident particle, mz is the mass of the stationary target particle, and m3,mi,
m5, and m6 are the product particle masses. For p production,
Ump)2c2-(2mp)2c2
v—v±
2= ( 6 ) ( 9 3 8 3 M e V ) = 5 6 3 0 M e V o r 5 6 3 G e V
K
= \—v±
= 6
p
2mT
- » M+ +
n
(Violates baryon number: 0 -> 0 + 1 , and violates
muon-lepton number: 0 -> -1 + 0.
M O D E R N PHYSICS
(b)
117
Using Equation 15.16 for the reaction p + p + n + n ,
(2mp + 2m„) c2 -(2m p ) c2
K.i, —
2m„
(4)[(938.8 + 939.6)2MeV2c2 -(4(938.3) 2 MeV 2 c 2 )] _
=
15-15
(2X938.3 MeV)
5.64 GeV
Let E = efficiency in %
m
x°C
For Example 15.5, E =
n
For Exercise 3, E =
xl00 =
xl00 =
\ %-th
135 MeV
xl00 = 48%
280 MeV J
139.6 MeV
x 100 = 48%
292 MeV
(m + c 2 ^
139.6 MeV
xl00 = 2
E=2 K
xl00 = 46%
600 MeV
V 2 ' xl00 = 2 938.3 MeV
For Problem 13, E = 2
K th J
5.63 GeV
x 100 = 33%
15-17
I ° + p ^ £ + + j'+X
dds+uud->uds+0+?
The left side has a net 3d, 2u, and Is. The right hand side has Id, lu, and Is leaving 2d and l u
missing. The unknown particle is a neutron, udd. Baryon and strangeness numbers are
conserved.
15-19
Quark composition of proton = uud, and of neutron = udd. Thus, if we neglect binding
energies, we may write:
mp=2mu+md
and mn=mu+ 2md
Solving simultaneously, we find:
m u = i ( 2 m p - m n ) =-[2(938.3 MeV/c 2 )-939.6 MeV/c 2 ] = 312.3 MeV/c 2 ,
and from either Equations (1) or (2), md = 313.6 MeV/c 2 . These should be compared to the
experimental masses mu - 5 MeV/c 2 and md =10 MeV/c 2 .
15-21
n = (u d
d)
time
ip = (u d
u)
Down quark
decays to an up quark
with the emission of a
virtual W minus.
(1)
(2)
%
118
CHAPTER 15
PARTICLE PHYSICS
15-23
A photon travels the distance from the Large Magellanic Cloud to us in 170 000 years. The
hypothetical massive neutrino travels the same distance in 170 000 years plus 10 seconds:
c(170 000 yr) = v(170 000 yr +10 s)
v_
170000 yr
c
170 000 yr +10 s
1
1
1 + (10 s/[(l.7x 10s yr)(3.156 x 107 s/yr)]}
1 +1.86 x 10"12
For the neutrino we want to evaluate mc2 in E = ymc2:
mc2 = - = EJI -~ = 10 MeV 1 •
: 10 MeV.
(l + 1.86xHT12)
|(l + 1.86xl0- 12 ) - 1
(l + 1.86xHT 12 ) 2
,
/2(l.86xl0- 12 )
mc2 «10 MeW—
'- = 10 MeV(l.93 x 10"6) = 19 eV
Then the upper limit on the mass is
m-
19 eV
19 eV
m=15-25
931.5 xlO 6 eV/c 2
= 2.1xl0" 8 u.
mAc* =1115.6 MeV
Au - > p + / r ~
mpc2 = 938.3 MeV (See Table 15.2 for masses)
m„c2= 139.6 MeV
The difference between starting mass-energy and final mass-energy is the kinetic energy of
the products.
Kp+K„= 37.7 MeV and pp = - p ,
Applying conservation of relativistic energy,
[(938.3 MeV) 2 +p2c2f/2 -938.3 MeV+[(139.6 MeV) 2 +p2c2f/2 -139.6 MeV = 37.7 MeV.
Solving the algebra yields ppc - -pnc -100.4 MeV. Then
K„
(mpc2) +(100.4 MeV)2
1/2
-mpc2=5.4MeV
K„ = [(139.6 MeV)2 + (100.4 MeV) 2 ]' -139.6 MeV = 32.3 MeV
15-27
Time-dilated lifetime.
T=rT0
0.9xl0"" 10 s
2
2 2
(l-v /c f
0.9xl0" 1 0 s
2 1/2
(1-(0.96) )
distance =(0.96)(3xl0 8 m/s)(3.214xl0" 10 s) = 9.3 cm
= 3.214 x l 0 " l o s
MODERN PHYSICS
15-29
p + p - » p + ;r + +X
Q = Mp+Mp-Mp-M^-Mx
(From conservation of momentum, particle X has zero momentum and thus zero kinetic
energy.)
Q = (2)(70.4 MeV) = 938.3 MeV + 938.3 MeV - 938.3 MeV -139.5 MeV - Mx
M x = 939.6 MeV
X must be a neutral baryon of rest mass 939.6 MeV/c 2 . Thus X is a neutron.
15-31
(a)
(b)
The mediator of this weak interaction is a Z° boson.
The mediator of a strong (quark-quark) interaction is a gluon.
15-33
(a)
AE = (m„ -mp -me)c2. From Appendix B,
AE = (1.008 665 u -1.078 25 u)931.5 MeV/u = 0.782 MeV
(b)
Assuming the neutron at rest, momentum is conserved, pp = pe relativistic energy
conserved, [{mpc2f + (p 2 c 2 )]
+[(m c c 2 ) 2 +(p 2 c 2 )]
= mnc2. Since pp = p e .
[(938.3 MeV)2 +{pc)zf2 +[(0.511 MeV)2 +{pc)2f2 =939.36 MeV
Solving the algebra pc = 1.19 MeV. If pec = ymevec = 1.19 MeV, then,
yve
1.19 MeV
x
„„„„ ,
v.
1—*- =
=
^ = 2.329 where x = - £ c
0.511 MeV ( l - x 2 ) V
c
x 2 =(l-x 2 )5.423
= ^- = 0.919
c
»,= 0.919c = 276 xlO 6 m/s
x
Then m„t>„
= >fneeuc =
v v
v
p
(1.19MeV)(l.6xlO -13 J/MeV)
•
5
3 x l 0 8 m/s
«n 0 (1.19 MeV)(l.6xlO -13 J/MeV)
m^Jl.
1
J
i = 3.80xl05 m/s
27
8
y
mpc (1.67xl0~ kg)(3xlO m/s)
u p = 380 km/s = 0.001266c
15-35
(c)
The electron is relativistic, the proton is not.
(a)
(1.602177 x lO"19 C)(1.15 T)(1.99 m) 686 MeV
p^=eBr.,--,
=
r,—
z
^
5.344 288 xlO - 2 2 (kg • m/s)/(MeV/c)
c
(1.602177xlO"19 C)(1.15 T)(0.580 m) _ 200 MeV
VK
" ~e *** ~ 5.344288xlO -22 (kg m/s)/(MeV/c) ~
c
120
CHAPTER 15
(b)
PARTICLE PHYSICS
Let #>be the angle made by the neutron's path with the path of the £ + at the moment
of decay. By conservation of momentum:
p„ cos <p+(199.961581 MeV/c) cos 64.5°=686.075 081 MeV/c
.-. p„ cos cp=599.989 401 MeV/c
(1)
p„ sin (p=(199.961581 MeV/c) sin 64.5°=180.482 380 MeV/c
(2)
From (1) and (2):
pn =V(599.989 401 MeV/c) 2 + (180.482380 MeV/c) 2 =627 MeV/c.
(c)
E ^ = -/(p^:) 2 + (m^ c2 f = V(199.961581 MeV) 2 + (139.6 MeV) 2 = 244 MeV
En = V(P»C)2 + ( m « c 2 ) 2 = V(626.547 022 MeV) 2 + (939.6 MeV)2 = 1130 MeV
ET+ = £ + + E = 243.870 445 MeV +1129.340 219 MeV = 1370 MeV
(d)
m r c 2 = ^E 2 + - ( p r c)2 = V(l 373.210 664 MeV) 2 - (686.075 081 MeV)2 -1190 MeV
. \ m r = 1190MeV/c 2
2
E_t =ym^c
z
z
.
f, u 2 V V 2 1373.210664 MeV , „ A A „ , . r
, where y= 1—z=
= 1.154 4. Solving for v,
5
1, c2)
1189.541303 MeV
o = 0.500c.
15-37
(a)
If 2N particles are annihilated, the energy released is 2Nmc2. The resulting photon
E 2Nmc2
...
momentum is p = — =
= 2Nmc. Smce the momentum of the system is
c
c
conserved, the rocket will have momentum 2Nmc directed opposite the photon
momentum, p = 2Nmc.
(b)
Consider a particle that is annihilated and gives up its rest energy mc2 to another
particle that also has initial rest energy mc2 (but no momentum initially).
E2=P2c2+(mc2)2
Thus (2mc2) = p2c2 +[mc2) . Where p is the momentum the second particle acquires
as a result of the annihilation of the first particle. Thus 4(mc2) = p2c2
+{mc2)2,
p2 = 3(mc2) . So p = V3mc. This process is repeated N times (annihilate — protons
N
and — antiprotons). Thus the total momentum acquired by the ejected particles is
V3Nmc, and this momentum is imparted to the rocket.
p = V3Nmc
(c)
Method (a) produces greater speed since 2Nmc > -j3Nmc.
STUDENT S LUTIONS MANUAL FOR
third
edition
\>^*
y r..
1
\
>
'
•
%
.
-
*
•
:
•
*
.
/
SERWAY / MOSES / MOYER
ft
lli